Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11483
Days in orbit
Revolutions
≈ 14.3
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: 1994-029AFF
Object number (NORAD): 39320
Object ID (CCSDS): 39320
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.551 minutes
Inclination: 81.7577 deg
SMA: 7162.83 km
Apoapsis: 987.566 km
Periapsis: 581.824 km
RAAN: 323.9139 deg
Eccentricy: 0.02832271
Argument of periapsis: 8.671 deg
Mean anomaly: 351.9217 deg
Mean motion: 14.32108033 rev/day
Mean motion (dot): 0.00003562 rev/day2
B* drag term: 0.00084457815 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 8:32 a.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39320U 94029AFF 25291.35564493 .00003562 00000-0 84458-3 0 9997
TLE line 2: 2 39320 81.7577 323.9139 0283227 8.6710 351.9217 14.32108033692639
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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