Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11373
Days in orbit
Revolutions
≈ 14.6
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: 1994-029AFD
Object number (NORAD): 39318
Object ID (CCSDS): 39318
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.362 minutes
Inclination: 81.9429 deg
SMA: 7058.471 km
Apoapsis: 813.399 km
Periapsis: 547.272 km
RAAN: 50.7394 deg
Eccentricy: 0.0188516
Argument of periapsis: 14.8574 deg
Mean anomaly: 359.212 deg
Mean motion: 14.63985751 rev/day
Mean motion (dot): 0.00001044 rev/day2
B* drag term: 0.00015027 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 9:28 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 39318U 94029AFD 25188.89467480 .00001044 00000-0 15027-3 0 9995
TLE line 2: 2 39318 81.9429 50.7394 0188516 14.8574 359.2120 14.63985751227681
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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