Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11368
Days in orbit
Revolutions
≈ 14.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
81.7
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: 1994-029AEZ
Object number (NORAD): 39314
Object ID (CCSDS): 39314
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.035 minutes
Inclination: 81.6552 deg
SMA: 7042.819 km
Apoapsis: 782.794 km
Periapsis: 546.574 km
RAAN: 239.9301 deg
Eccentricy: 0.0167703
Argument of periapsis: 173.4937 deg
Mean anomaly: 186.8505 deg
Mean motion: 14.68868617 rev/day
Mean motion (dot): 0.00002921 rev/day2
B* drag term: 0.00039981 1/REarth
Two-line elements (TLE)
Creation date: June 29, 2025, 2:41 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 28, 2025, 9:42 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39314U 94029AEZ 25179.90458736 .00002921 00000-0 39981-3 0 9997
TLE line 2: 2 39314 81.6552 239.9301 0167703 173.4937 186.8505 14.68868617608781
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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