pypredict 1.6.3

Interface to the Predict satellite tracking and orbital prediction library

PyPredict

NOTE: To preserve compatibility with predict, pypredict uses north latitude and west longitude for terrestrial coordinates.

Do you want accurate and time-tested satellite tracking and pass prediction in a convenient python wrapper? You're in the right place.

PyPredict is a C Python extension directly adapted from the ubiquitous predict satellite tracking command line application. Originally written for the commodore 64, predict has a proven pedigree; We just aim to provide a convenient API. PyPredict is a port of the predict codebase and should yield identical results.

If you think you've found an error in pypredict, please include output from predict on same inputs to the bug report.
If you think you've found a bug in predict, please report and we'll coordinate with upstream.

Installation

sudo apt-get install python-dev
sudo python setup.py install

Usage

Observe a satellite (relative to a position on earth)

import predict
tle = """0 LEMUR 1
1 40044U 14033AL  15013.74135905  .00002013  00000-0  31503-3 0  6119
2 40044 097.9584 269.2923 0059425 258.2447 101.2095 14.72707190 30443"""
qth = (37.771034, 122.413815, 7)  # lat (N), long (W), alt (meters)
predict.observe(tle, qth) # optional time argument defaults to time.time()
# => {'altitude': 676.8782276657903,
#     'azimuth': 96.04762045174824,
#     'beta_angle': -27.92735429908726,
#     'decayed': 0,
#     'doppler': 1259.6041017128405,
#     'eci_obs_x': -2438.227652191655,
#     'eci_obs_y': -4420.154476060397,
#     'eci_obs_z': 3885.390601342013,
#     'eci_sun_x': 148633398.020844,
#     'eci_sun_y': -7451536.44122029,
#     'eci_sun_z': -3229999.50056359,
#     'eci_vx': 0.20076213530665032,
#     'eci_vy': -1.3282146055077213,
#     'eci_vz': 7.377067234096598,
#     'eci_x': 6045.827328897242,
#     'eci_y': -3540.5885778261277,
#     'eci_z': -825.4065096776636,
#     'eclipse_depth': -87.61858291647795,
#     'elevation': -43.711904591801726,
#     'epoch': 1521290038.347793,
#     'footprint': 5633.548906707907,
#     'geostationary': 0,
#     'has_aos': 1,
#     'latitude': -6.759563817939698,
#     'longitude': 326.1137007912563,
#     'name': '0 LEMUR 1',
#     'norad_id': 40044,
#     'orbit': 20532,
#     'orbital_model': 'SGP4',
#     'orbital_phase': 145.3256815318047,
#     'orbital_velocity': 26994.138671706416,
#     'slant_range': 9743.943478523843,
#     'sunlit': 1,
#     'visibility': 'D'
#    }

Show upcoming transits of satellite over groundstation

p = predict.transits(tle, qth)
for _ in xrange(10):
	transit = p.next()
	print("%f\t%f\t%f" % (transit.start, transit.duration(), transit.peak()['elevation']))

Call predict analogs directly

predict.quick_find(tle.split('\n'), time.time(), (37.7727, 122.407, 25))
predict.quick_predict(tle.split('\n'), time.time(), (37.7727, 122.407, 25))

API

observe(tle, qth[, at=None])  
    Return an observation of a satellite relative to a groundstation.
    qth groundstation coordinates as (lat(N),long(W),alt(m))
    If at is not defined, defaults to current time (time.time())
    Returns an "observation" or dictionary containing:  
        altitude _ altitude of satellite in kilometers
        azimuth - azimuth of satellite in degrees from perspective of groundstation.
        beta_angle
        decayed - 1 if satellite has decayed out of orbit, 0 otherwise.
        doppler - doppler shift between groundstation and satellite.
        eci_obs_x
        eci_obs_y
        eci_obs_z
        eci_sun_x
        eci_sun_y
        eci_sun_z
        eci_vx
        eci_vy
        eci_vz
        eci_x
        eci_y
        eci_z
        eclipse_depth
        elevation - elevation of satellite in degrees from perspective of groundstation.
        epoch - time of observation in seconds (unix epoch)
        footprint
        geostationary - 1 if satellite is determined to be geostationary, 0 otherwise.
        has_aos - 1 if the satellite will eventually be visible from the groundstation
        latitude - north latitude of point on earth directly under satellite.
        longitude - west longitude of point on earth directly under satellite.
        name - name of satellite from first line of TLE.
        norad_id - NORAD id of satellite.
        orbit
        orbital_phase
        orbital_model
        orbital_velocity
        slant_range - distance to satellite from groundstation in meters.
        sunlit - 1 if satellite is in sunlight, 0 otherwise.
        visibility
transits(tle, qth[, ending_after=None][, ending_before=None])  
    Returns iterator of Transit objects representing passes of tle over qth.  
    If ending_after is not defined, defaults to current time  
    If ending_before is not defined, the iterator will yield until calculation failure.

NOTE: We yield passes based on their end time. This means we'll yield currently active passes in the two-argument invocation form, but their start times will be in the past.

Transit(tle, qth, start, end)  
    Utility class representing a pass of a satellite over a groundstation.
    Instantiation parameters are parsed and made available as fields.
    duration()  
        Returns length of transit in seconds
    peak(epsilon=0.1)  
        Returns epoch time where transit reaches maximum elevation (within ~epsilon)
    at(timestamp)  
        Returns observation during transit via quick_find(tle, timestamp, qth)
quick_find(tle[, time[, (lat, long, alt)]])  
    time defaults to current time   
    (lat, long, alt) defaults to values in ~/.predict/predict.qth  
    Returns observation dictionary equivalent to observe(tle, time, (lat, long, alt))
quick_predict(tle[, time[, (lat, long, alt)]])  
        Returns an array of observations for the next pass as calculated by predict.
        Each observation is identical to that returned by quick_find.