Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11485
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
LEO
Low Earth Orbit
Inclination
81.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for PEGASUS DEB.
Object identification
Identified? True
Debris? True
Object name: PEGASUS DEB
International designator: 1994-029AEV
Object number (NORAD): 39310
Object ID (CCSDS): 39310
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.28 minutes
Inclination: 81.8133 deg
SMA: 7102.341 km
Apoapsis: 893.438 km
Periapsis: 554.973 km
RAAN: 299.3739 deg
Eccentricy: 0.02382771
Argument of periapsis: 2.5319 deg
Mean anomaly: 357.7017 deg
Mean motion: 14.50442452 rev/day
Mean motion (dot): 0.00007756 rev/day2
B* drag term: 0.0013697415 1/REarth
Two-line elements (TLE)
Creation date: Oct. 16, 2025, 2:37 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 15, 2025, 6:49 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39310U 94029AEV 25288.78466150 .00007756 00000-0 13697-2 0 9995
TLE line 2: 2 39310 81.8133 299.3739 0238277 2.5319 357.7017 14.50442452808718
Live tracking on map
Real-time ground track for satellite PEGASUS DEB.
Associated space launch
PEGASUS DEB was lifted into orbit during the mission ‘Pegasus HAPS | Space Test Experiments Platform 2 (STEP-2)’, on board a Pegasus HAPS space rocket.
The launch took place on May 19, 1994, 5:03 p.m. from Edwards Air Force Base.
For more information about the launch, click the button.
Pegasus HAPS | Space Test Experiments Platform 2 (STEP-2)
Agency: N/A
Status: Launch Successful
Launch date: May 19, 1994, 5:03 p.m. UTC
Rocket: Pegasus HAPS
Launch pad: Edwards Air Force Base
Location: Air launch to orbit
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