Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11487
Days in orbit
Revolutions
≈ 15.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
81.9
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: 1994-029AES
Object number (NORAD): 39307
Object ID (CCSDS): 39307
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 95.181 minutes
Inclination: 81.9444 deg
SMA: 6905.458 km
Apoapsis: 597.194 km
Periapsis: 457.452 km
RAAN: 115.8139 deg
Eccentricy: 0.0101182
Argument of periapsis: 195.2329 deg
Mean anomaly: 164.585 deg
Mean motion: 15.12913354 rev/day
Mean motion (dot): 0.00038703 rev/day2
B* drag term: 0.001929 1/REarth
Two-line elements (TLE)
Creation date: Oct. 27, 2025, 6:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 26, 2025, 10:28 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39307U 94029AES 25299.93662524 .00038703 00000-0 19290-2 0 9994
TLE line 2: 2 39307 81.9444 115.8139 0101182 195.2329 164.5850 15.12913354748053
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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