SpacePy: Space Science Tools for Python

SpacePy is a package of tools primarily aimed at the space science community. This __init__.py file sets the parameters for import statements.

If running the ipython shell, simply type ‘?’ after any command for help. ipython also offers tab completion, so hitting tab after ‘<module name>.’ will list all available functions, classes and variables.

Detailed HTML documentation is available locally in the spacepy/doc directory and can be launched by typing:

>>> spacepy.help()

Most functionality is in spacepy’s submodules. Each module has specific help available:

Submodules

coordinates	Implementation of Coords class functions for coordinate transformations
data_assimilation
datamodel	The datamodel classes constitute a data model implementation meant to mirror the functionality of the data model output from pycdf, though implemented slightly differently.
empiricals	Module with some useful empirical models (plasmapause, magnetopause, Lmax)
irbempy	module wrapper for irbem_lib Reference for this library https://sourceforge.net/projects/irbem/ D.
LANLstar	Lstar and Lmax calculation using artificial neural network (ANN) technique.
omni	Tools to read and process omni data (Qin-Denton, etc.)
poppy	PoPPy – Point Processes in Python.
pybats	PyBats! An open source Python-based interface for reading, manipulating, and visualizing BATS-R-US and SWMF output.
pycdf	This package provides a Python interface to the Common Data Format (CDF) library used for many NASA missions, available at http://cdf.gsfc.nasa.gov/.
radbelt	Functions supporting radiation belt diffusion codes
seapy	SeaPy – Superposed Epoch in Python.
time	Time conversion, manipulation and implementation of Ticktock class
toolbox	Toolbox of various functions and generic utilities.
ae9ap9	Module for reading and dealing with AE9AP9 data files.

Functions

deprecated(version, message[, docstring])	Decorator to deprecate a function/method
help()	Launches web browser with local HTML help

spacepy.deprecated(version, message, docstring=None)

Decorator to deprecate a function/method

Modifies a function so that calls to it raise DeprecationWarning and the docstring has a deprecation note added in accordance with numpydoc format

Parameters

versionstr

What is the first version where this was deprecated?

messagestr

Message to include in the deprecation warning and in the docstring.

Other Parameters

docstringstr

New in version 0.2.2.

If specified, docstring will be added to the modified function’s docstring instead of message (which will only be used in the deprecation warning.) It can be a multi-line string (separated with \n). It will be indented to match the existing docstring.

Notes

On Python 2, the deprecated function’s signature won’t be preserved. The function will work but will not have proper argument names listed in e.g. help.

Examples

>>> import spacepy
>>> @spacepy.deprecated('0.2.1', 'Use a different function instead',
...                     docstring='A different function is better\n'
...                               'because of reasons xyz')
... def foo(x):
...     '''This is a test function
...
...     It may do many useful things.
...     '''
...     return x + 1
>>> help(foo)
Help on function foo in module __main__:
foo(x)
    This is a test function
    .. deprecated:: 0.2.1
       A different function is better
       because of reasons xyz
    It may do many useful things.
>>> foo(2)
DeprecationWarning: Use a different function instead
3

spacepy.help()

Launches web browser with local HTML help

Copyright 2010-2016 Los Alamos National Security, LLC.

SpacePy - A Quick Start Documentation

The SpacePy Team (Steve Morley, Josef Koller, Dan Welling, Brian Larsen, Jon Niehof, Mike Henderson)

Installation

See Installing SpacePy.

Toolbox - A Box Full of Tools

Contains tools that don’t fit anywhere else but are, in general, quite useful. The following functions are a selection of those implemented:

• windowMean(): windowing mean with variable window size and overlap

• dictree(): pretty prints the contents of dictionaries (recursively)

• loadpickle(): single line convenience routine for loading Python pickles

• savepickle(): same as loadpickle, but for saving

• update(): updates the OMNI database and the leap seconds database (internet connection required)

• tOverlap(): find interval of overlap between two time series

• tCommon(): find times common to two time series

• binHisto(): calculate number of bins for a histogram

• medAbsDev(): find the median absolute deviation of a data series

• normalize(): normalize a data series

• feq(): floating point equals

Import this module as:

>>> import spacepy.toolbox as tb

Examples:

>>> import spacepy.toolbox as tb
>>> a = {'entry1':'val1', 'entry2':2, 'recurse1':{'one':1, 'two':2}}
>>> tb.dictree(a)
+
|____entry1
|____entry2
|____recurse1
     |____one
     |____two
>>> import numpy as np
>>> dat = np.random.random_sample(100)
>>> tb.binHisto(dat)
(0.19151723370512266, 5.0)

Time and Coordinate Transformations

Import the modules as:

>>> import spacepy.time as spt
>>> import spacepy.coords as spc

Ticktock Class

The Ticktock class provides a number of time conversion routines and is implemented as a container class built on the functionality of the Python datetime module. The following time coordinates are provided

• UTC: Coordinated Universal Time implemented as a datetime.datetime

• ISO: standard ISO 8601 format like 2002-10-25T14:33:59

• TAI: International Atomic Time in units of seconds since Jan 1, 1958 (midnight) and includes leap seconds, i.e. every second has the same length

• JD: Julian Day

• MJD: Modified Julian Day

• UNX: UNIX time in seconds since Jan 1, 1970

• RDT: Rata Die Time (Gregorian Ordinal Time) in days since Jan 1, 1 AD midnight

• CDF: CDF Epoch time in milliseconds since Jan 1, year 0

• DOY: Day of Year including fractions

• leaps: Leap seconds according to ftp://maia.usno.navy.mil/ser7/tai-utc.dat

To access these time coordinates, you’ll create an instance of a Ticktock class, e.g.:

>>> t = spt.Ticktock('2002-10-25T12:30:00', 'ISO')

Instead of ISO you may use any of the formats listed above. You can also use numpy arrays or lists of time points. t has now the class attributes:

>>> t.dtype = 'ISO'
>>> t.data = '2002-10-25T12:30:00'

FYI t.UTC is added automatically.

If you want to convert/add a class attribute from the list above, simply type e.g.:

>>> t.RTD

You can replace RTD with any from the list above.

You can find out how many leap seconds were used by issuing the command:

>>> t.getleapsecs()

Timedelta Class

You can add/subtract time from a Ticktock class instance by using an instance of datetime.timedelta:

>>> dt = datetime.timedelta(days=2.3)

Then you can add by e.g.:

>>> t+dt

Coords Class

The spatial coordinate class includes the following coordinate systems in Cartesian and spherical forms.

• GZD: (altitude, latitude, longitude) in km, deg, deg

• GEO: cartesian, Re

• GSM: cartesian, Re

• GSE: cartesian, Re

• SM: cartesian, Re

• GEI: cartesian, Re

• MAG: cartesian, Re

• SPH: same as GEO but in spherical

• RLL: radial distance, latitude, longitude, Re, deg, deg.

Create a Coords instance with spherical=’sph’ or cartesian=’car’ coordinates:

>>> spaco = spc.Coords([[1,2,4],[1,2,2]], 'GEO', 'car')

This will let you request, for example, all y-coordinates by spaco.y or if given in spherical coordinates by spaco.lati. One can transform the coordinates by newcoord = spaco.convert('GSM', 'sph'). This will return GSM coordinates in a spherical system. Since GSM coordinates depend on time, you’ll have to add first a Ticktock vector with the name ticks like spaco.ticks = spt.Ticktock(['2002-02-02T12:00:00', '2002-02-02T12:00:00'], 'ISO')

Unit conversion will be implemented in the future.

The radbelt Module

The radiation belt module currently includes a simple radial diffusion code as a class. Import the module and instatiate a radbelt object:

>>> import spacepy.radbelt as sprb
>>> rb = sprb.RBmodel()

Add a time grid for a particular period that you are interested in:

>>> rb.setup_ticks('2002-02-01T00:00:00', '2002-02-10T00:00:00', 0.25)

This will automatically lookup required geomagnetic/solar wind conditions for that period. Run the diffusion solver for that setup and plot the results:

>>> rb.evolve()
>>> rb.plot()

The Data Assimilation Module

This module includes data assimilation capabilities, through the assimilation class. The class assimilates data for the radiation belt model using the Ensemble Kalman Filter. The algorithm used is the SVD method presented by Evensen in 2003 (Evensen, G., Ocean dynamics, 53, pp.343–367, 2003). To compensate for model errors, three inflation algorithms are implemented. The inflation methodology is specified by the inflation argument, where the options are the following:

• inflation = 0: Add model error (perturbation for the ensemble) around model state values only where observations are available (DEFAULT).

• inflation = 1: Add model error (perturbation for the ensemble) around observation values only where observations are available.

• inflation = 2: Inflate around ensemble average for EnKF.

Prior to assimilation, a set of data values has to be specified by setting the start and end dates, and time step, using the setup_ticks function of the radiation belt model:

>>> import spacepy
>>> import datetime
>>> from spacepy import radbelt

>>> start = datetime.datetime(2002,10,23)
>>> end = datetime.datetime(2002,11,4)
>>> delta = datetime.timedelta(hours=0.5)
>>> rmod.setup_ticks(start, end, delta, dtype='UTC')

Once the dates and time step are specified, the data is added using the add_PSD function (NOTE: This requires a database available from the SpacePy team):

>>> rmod.add_PSD()

The observations are averaged over the time windows, whose interval is give by the time step. Once the dates and data are set, the assimilation is performed using the assimilate function:

>>> rmod.assimilate(inflation=1)

This function will add the PSDa values, which are the analysis state of the radiation belt using the observations within the dates. To plot the analysis simply use the plot function:

>>> rmod.plot(values=rmod.PSDa,clims=[-10,-6],Lmax=False,Kp=False,Dst=False)

Additionally, to create a summary plot of the observations use the plot_obs function within the radbelt module. For reference, the last closed drift shell, Dst, and Kp are all included. These can be disabled individually using the corresponding Boolean kwargs.

The clims kwarg can be used to manually set the color bar range. To use, set it equal to a two-element list containing minimum and maximum log ₁₀ value to plot. Default action is to use [0,10] as the log ₁₀ of the color range. This is good enough for most applications. The title of the top most plot defaults to ‘Summary Plot’ but can be customized using the title kwarg.

The figure object and all three axis objects (PSD axis, Dst axis, and Kp axis) are all returned to allow the user to further customize the plots as necessary. If any of the plots are excluded, None is returned in their stead.

Example:

>>> rmod.plot_obs(clims=[-10,-6],Lmax=False,Kp=False,Dst=False,title='Observations Plot')

This command would create the summary plot with a color bar range of 10 ^-10 to 10 ^-6. The Lmax line, Kp and Dst values would be excluded. The title of the topmost plot (phase space density) would be set to ‘Observations Plot’.

OMNI Module

The OMNI database is an hourly resolution, multi-source data set with coverage from November 1963; higher temporal resolution versions of the OMNI database exist, but with coverage from 1995. The primary data are near-Earth solar wind, magnetic field and plasma parameters. However, a number of modern magnetic field models require derived input parameters, and Qin and Denton (2007) have used the publicly-available OMNI database to provide a modified version of this database containing all parameters necessary for these magnetic field models. These data are available through ViRBO - the Virtual Radiation Belt Observatory.

In SpacePy this data is made available, at 1-hourly resolution, on request on first import; if not downloaded when SpacePy is first used then any attempt to import the omni module will ask the user whether they wish to download the data. Should the user require the latest data, the toolbox.update function can be used to fetch the latest files from ViRBO.

The following example fetches the OMNI data for the storms of October and November, 2003.:

>>> import spacepy.time as spt
>>> import spacepy.omni as om
>>> import datetime as dt
>>> st = dt.datetime(2003,10,20)
>>> en = dt.datetime(2003,12,5)
>>> delta = dt.timedelta(days=1)
>>> ticks = spt.tickrange(st, en, delta, 'UTC')
>>> data = om.get_omni(ticks)

data is a dictionary containing all the OMNI data, by variable, for the timestamps contained within the Ticktock object ticks. Now it is simple to plot Dst values for instance:

>>> import pyplot as p
>>> p.plot(ticks.eDOY, data['Dst'])

The irbempy Module

ONERA (Office National d’Etudes et Recherches Aerospatiales) initiated a well-known FORTRAN library that provides routines to compute magnetic coordinates for any location in the Earth’s magnetic field, to perform coordinate conversions, to compute magnetic field vectors in geospace for a number of external field models, and to propagate satellite orbits in time. Older versions of this library were called ONERA-DESP-LIB. Recently the library has changed its name to IRBEM-LIB and is maintained by a number of different institutions.

A number of key routines in IRBEM-LIB have been made available through the module irbempy. Current functionality includes calls to calculate the local magnetic field vectors at any point in geospace, calculation of the magnetic mirror point for a particle of a given pitch angle (the angle between a particle’s velocity vector and the magnetic field line that it immediately orbits such that a pitch angle of 90 degrees signifies gyration perpendicular to the local field) anywhere in geospace, and calculation of electron drift shells in the inner magnetosphere.:

>>> import spacepy.time as spt
>>> import spacepy.coordinates as spc
>>> import spacepy.irbempy as ib
>>> t = spt.Ticktock(['2002-02-02T12:00:00', '2002-02-02T12:10:00'], 'ISO')
>>> y = spc.Coords([[3,0,0],[2,0,0]], 'GEO', 'car')
>>> ib.get_Bfield(t,y)
>>> # {'Blocal': array([  976.42565251,  3396.25991675]),
>>> #    'Bvec': array([[ -5.01738885e-01,  -1.65104338e+02,   9.62365503e+02], [  3.33497974e+02,  -5.42111173e+02,   3.33608693e+03]])}

One can also calculate the drift shell L* for a 90 degree pitch angle value by using:

>>> ib.get_Lstar(t,y, [90])
>>> # {'Bmin': array([  975.59122652,  3388.2476667 ]),
>>> #  'Bmirr': array([[  976.42565251], [ 3396.25991675]]),
>>> #  'Lm': array([[ 3.13508015], [ 2.07013638]]),
>>> #  'Lstar': array([[ 2.86958324], [ 1.95259007]]),
>>> #  'MLT': array([ 11.97222034,  12.13378624]),
>>> #  'Xj': array([[ 0.00081949], [ 0.00270321]])}

Other function wrapped with the IRBEM library include:

• find_Bmirror()

• find_magequator()

• coord_trans()

pyCDF - Python Access to NASA CDF Library

pycdf provides a “pythonic” interface to the NASA CDF library. It requires that the NASA CDF C-library is properly installed. The module can then be imported, e.g.:

>>> import spacepy.pycdf as cdf

To open and close a CDF file, we use the CDF class:

>>> cdf_file = cdf.CDF('filename.cdf')
>>> cdf_file.close()

CDF files, like standard Python files, act as context managers:

>>> with cdf.CDF('filename.cdf') as cdf_file:
>>>     #do brilliant things with cdf_file
>>> #cdf_file is automatically closed here

CDF files act as Python dictionaries, holding CDF variables keyed by the variable name:

>>> var_names = keys(cdf_file) #list of all variables
>>> for var_name in cdf_file:
>>>     print(len(cdf_file[var_name])) #number of records in each variable
>>> #list comprehensions work, too
>>> lengths = [len(cdf_file[var_name]) for var_name in cdf_file]

Each CDF variable acts like a numpy array, where the first dimension is the record number. Multidimensional CDF variables can be subscripted using numpy’s multidimensional slice notation. Many common list operations are also implemented, where each record acts as one element of the list and can be independently deleted, inserted, etc. Creating a Python Var object does not read the data from disc; data are only read as they are accessed:

>>> epoch = cdf_file['Epoch'] #Python object created, nothing read from disc
>>> epoch[0] #time of first record in CDF (datetime object)
>>> a = epoch[...] #copy all times to list a
>>> a = epoch[-5:] #copy last five times to list a
>>> b_gse = cdf_file['B_GSE'] #B_GSE is a 1D, three-element array
>>> bz = b_gse[0,2] #Z component of first record
>>> bx = b_gse[:,0] #copy X component of all records to bx
>>> bx = cdf_file['B_GSE'][:,0] #same as above

The datamodel Module

The SpacePy datamodel module implements classes that are designed to make implementing a standard data model easy. The concepts are very similar to those used in standards like HDF5, netCDF and NASA CDF.

The basic container type is analogous to a folder (on a filesystem; HDF5 calls this a group): Here we implement this as a dictionary-like object, a datamodel.SpaceData object, which also carries attributes. These attributes can be considered to be global, i.e. relevant for the entire folder. The next container type is for storing data and is based on a numpy array, this class is datamodel.dmarray and also carries attributes. The dmarray class is analogous to an HDF5 dataset.

Guide for NASA CDF users

By definition, a NASA CDF only has a single ‘layer’. That is, a CDF contains a series of records (stored variables of various types) and a set of attributes that are either global or local in scope. Thus to use SpacePy’s datamodel to capture the functionality of CDF the two basic data types are all that is required, and the main constraint is that datamodel.SpaceData objects cannot be nested (more on this later, if conversion from a nested datamodel to a flat datamodel is required).

This is best illustrated with an example. Imagine representing some satellite data within a CDF – the global attributes might be the mission name and the instrument PI, the variables might be the instrument counts [n-dimensional array], timestamps[1-dimensional array and an orbit number [scalar]. Each variable will have one attribute (for this example).

>>> import spacepy.datamodel as dm
>>> mydata = dm.SpaceData(attrs={'MissionName': 'BigSat1'})
>>> mydata['Counts'] = dm.dmarray([[42, 69, 77], [100, 200, 250]], attrs={'Units': 'cnts/s'})
>>> mydata['Epoch'] = dm.dmarray([1, 2, 3], attrs={'units': 'minutes'})
>>> mydata['OrbitNumber'] = dm.dmarray(16, attrs={'StartsFrom': 1})
>>> mydata.attrs['PI'] 'Prof. Big Shot'

This has now populated a structure that can map directly to a NASA CDF. To visualize our datamodel, we can use the tree() method, which is equivalent to toolbox.dictree() (which works for any dictionary-like object, including PyCDF file objects).

>>> mydata.tree(attrs=True)
+
:|____MissionName
:|____PI
|____Counts
    :|____Units
|____Epoch
    :|____units
|____OrbitNumber
    :|____StartsFrom
>>> import spacepy.toolbox as tb
>>> tb.dictree(mydata, attrs=True)
+
:|____MissionName
:|____PI
|____Counts
    :|____Units
|____Epoch
    :|____units
|____OrbitNumber
    :|____StartsFrom

Attributes are denoted by a leading colon. The global attributes are those in the base level, and the local attributes are attached to each variable.

If we have data that has nested ‘folders’, allowed by HDF5 but not by NASA CDF, then how can this be represented such that the data structure can be mapped directly to a NASA CDF? The data will need to be flattened so that it is single layered. Let us now store some ephemerides in our data structure:

>>> mydata['Ephemeris'] = dm.SpaceData()
>>> mydata['Ephemeris']['GSM'] = dm.dmarray([[1,3,3], [1.2,4,2.5], [1.4,5,1.9]])
>>> tb.dictree(mydata, attrs=True)
+
:|____MissionName
:|____PI
|____Counts
    :|____Units
|____Ephemeris
    |____GSM
|____Epoch
    :|____units
|____OrbitNumber
    :|____StartsFrom

Nested dictionary-like objects is not uncommon in Python (and can be exceptionally useful for representing data, so to make this compatible with NASA CDF we call the flatten() method .

>>> mydata.flatten()
>>> tb.dictree(mydata, attrs=True)
+
:|____MissionName
:|____PI
|____Counts
    :|____Units
|____Ephemeris<--GSM
|____Epoch
    :|____units
|____OrbitNumber
    :|____StartsFrom

Note that the nested SpaceData has been moved to a variable with a new name reflecting its origin. The data structure is now flat again and can be mapped directly to NASA CDF.

Converters to/from datamodel

Currently converters exist to read HDF5 and NASA CDF files directly to a SpacePy datamodel. This capability also exists for JSON-headed ASCII files (RBSP/AutoPlot-compatible). A converter from the datamodel to HDF5 is now available and a converter to NASA CDF is under development. Also under development is the reverse of the SpaceData.flatten method, so that flattened objects can be restored to their former glory.

Empiricals Module

The empiricals module provides access to some useful empirical models. As of SpacePy 0.1.2, the models available are:

• getLmax() An empirical parametrization of the L* of the last closed drift shell (Lmax)

• getPlasmaPause() The plasmapause location, following either Carpenter and Anderson (1992) or Moldwin et al. (2002)

• getMPstandoff() The magnetopause standoff location (i.e. the sub-solar point), using the Shue et al. (1997) model

• vampolaPA() A conversion of omnidirectional electron flux to pitch-angle dependent flux, using the sin ⁿ model of Vampola (1996)

Each of the first three models is called by passing it a Ticktock object (see above) which then calculates the model output using the 1-hour Qin-Denton OMNI data (from the OMNI module; see above). For example:

>>> import spacepy.time as spt
>>> import spacepy.empiricals as emp
>>> ticks = spt.tickrange('2002-01-01T12:00:00','2002-01-04T00:00:00',.25)

calls tickrange() and makes a Ticktock object with times from midday on January 1st 2002 to midnight January 4th 2002, incremented 6-hourly:

>>> Lpp = emp.getPlasmaPause(ticks)

then returns the model plasmapause location using the default setting of the Moldwin et al. (2002) model. The Carpenter and Anderson model can be used by setting the Lpp_model keyword to ‘CA1992’.

The magnetopause standoff location can be called using this syntax, or can be called for specific solar wind parameters (ram pressure, P, and IMF Bz) passed through in a Python dictionary:

>>> data = {'P': [2,4], 'Bz': [-2.4, -2.4]}
>>> emp.getMPstandoff(data)
>>>   # array([ 10.29156018,   8.96790412])

SeaPy - Superposed Epoch Analysis in Python

Superposed epoch analysis is a technique used to reveal consistent responses, relative to some repeatable phenomenon, in noisy data . Time series of the variables under investigation are extracted from a window around the epoch and all data at a given time relative to epoch forms the sample of events at that lag. The data at each time lag are then averaged so that fluctuations not consistent about the epoch cancel. In many superposed epoch analyses the mean of the data at each time u relative to epoch, is used to represent the central tendency. In SeaPy we calculate both the mean and the median, since the median is a more robust measure of central tendency and is less affected by departures from normality. SeaPy also calculates a measure of spread at each time relative to epoch when performing the superposed epoch analysis; the interquartile range is the default, but the median absolute deviation and bootstrapped confidence intervals of the median (or mean) are also available.

As an example we fetch OMNI data for 4 years and perform a superposed epoch analysis of the solar wind radial velocity, with a set of epoch times read from a text file:

>>> import datetime as dt
>>> import spacepy.seapy as sea
>>> import spacepy.omni as om
>>> import spacepy.toolbox as tb
>>> import spacepy.time as spt
>>> # now read the epochs for the analysis (the path specified is the default
>>> # install location on linux, different OS will have this elsewhere)
>>> epochs = sea.readepochs('~/.local/lib/python2.7/site-packages/spacepy/data/SEA_epochs_OMNI.txt')

The readepochs function can handle multiple formats by a user-specified format code. ISO 8601 format is directly supported though it is not used here. The the readepochs docstring for more information. As above, we use the get_omni function to retrieve the hourly data from the OMNI module:

>>> ticks = spt.tickrange(dt.datetime(2005,1,1), dt.datetime(2009,1,1), dt.timedelta(hours=1))
>>> omni1hr = om.get_omni(ticks)
>>> omni1hr.tree(levels=1, verbose=True)

+
|____ByIMF (spacepy.datamodel.dmarray (35065,))
|____Bz1 (spacepy.datamodel.dmarray (35065,))
|____Bz2 (spacepy.datamodel.dmarray (35065,))
|____Bz3 (spacepy.datamodel.dmarray (35065,))
|____Bz4 (spacepy.datamodel.dmarray (35065,))
|____Bz5 (spacepy.datamodel.dmarray (35065,))
|____Bz6 (spacepy.datamodel.dmarray (35065,))
|____BzIMF (spacepy.datamodel.dmarray (35065,))
|____DOY (spacepy.datamodel.dmarray (35065,))
|____Dst (spacepy.datamodel.dmarray (35065,))
|____G (spacepy.datamodel.dmarray (35065, 3))
|____Hr (spacepy.datamodel.dmarray (35065,))
|____Kp (spacepy.datamodel.dmarray (35065,))
|____Pdyn (spacepy.datamodel.dmarray (35065,))
|____Qbits (spacepy.datamodel.SpaceData [7])
|____RDT (spacepy.datamodel.dmarray (35065,))
|____UTC (spacepy.datamodel.dmarray (35065,))
|____W (spacepy.datamodel.dmarray (35065, 6))
|____Year (spacepy.datamodel.dmarray (35065,))
|____akp3 (spacepy.datamodel.dmarray (35065,))
|____dens (spacepy.datamodel.dmarray (35065,))

and these data are used for the superposed epoch analysis. the temporal resolution is 1 hr and the window is +/- 3 days

>>> delta = dt.timedelta(hours=1)
>>> window= dt.timedelta(days=3)
>>> sevx = sea.Sea(omni1hr['velo'], omni1hr['UTC'], epochs, window, delta)
    #rather than quartiles, we calculate the 95% confidence interval on the median
>>> sevx.sea(ci=True)
>>> sevx.plot()