Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11435
Days in orbit
Revolutions
≈ 14.5
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: 1994-029AEV
Object number (NORAD): 39310
Object ID (CCSDS): 39310
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.325 minutes
Inclination: 81.8179 deg
SMA: 7104.491 km
Apoapsis: 898.068 km
Periapsis: 554.644 km
RAAN: 344.3424 deg
Eccentricy: 0.0241695
Argument of periapsis: 144.2024 deg
Mean anomaly: 217.5649 deg
Mean motion: 14.49783945 rev/day
Mean motion (dot): 0.00011807 rev/day2
B* drag term: 0.0020966844 1/REarth
Two-line elements (TLE)
Creation date: Aug. 31, 2025, 2:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 30, 2025, 1:18 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39310U 94029AEV 25242.55475051 .00011807 00000-0 20967-2 0 9990
TLE line 2: 2 39310 81.8179 344.3424 0241695 144.2024 217.5649 14.49783945802019
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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