Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11532
Days in orbit
Revolutions
≈ 14.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
82.0
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: 1994-029AEX
Object number (NORAD): 39312
Object ID (CCSDS): 39312
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.115 minutes
Inclination: 81.9786 deg
SMA: 7046.685 km
Apoapsis: 810.963 km
Periapsis: 526.137 km
RAAN: 230.7771 deg
Eccentricy: 0.02020997
Argument of periapsis: 56.2657 deg
Mean anomaly: 305.7624 deg
Mean motion: 14.6766006 rev/day
Mean motion (dot): 0.00010597 rev/day2
B* drag term: 0.0013628619 1/REarth
Two-line elements (TLE)
Creation date: Nov. 16, 2025, 11:15 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Nov. 14, 2025, 12:04 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39312U 94029AEX 25318.50327769 .00010597 00000-0 13629-2 0 9995
TLE line 2: 2 39312 81.9786 230.7771 0202100 56.2657 305.7624 14.67660060657575
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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