Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11532
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: 97.891 minutes
Inclination: 81.6566 deg
SMA: 7035.949 km
Apoapsis: 771.399 km
Periapsis: 544.229 km
RAAN: 77.6608 deg
Eccentricy: 0.0161435
Argument of periapsis: 33.2619 deg
Mean anomaly: 327.8605 deg
Mean motion: 14.71020613 rev/day
Mean motion (dot): 0.00009659 rev/day2
B* drag term: 0.00128 1/REarth
Two-line elements (TLE)
Creation date: Dec. 4, 2025, 9:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 4, 2025, 2:08 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39314U 94029AEZ 25338.58929924 .00009659 00000-0 12800-2 0 9995
TLE line 2: 2 39314 81.6566 77.6608 0161435 33.2619 327.8605 14.71020613632098
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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