Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11532
Days in orbit
Revolutions
≈ 14.3
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: 1994-029AEJ
Object number (NORAD): 27679
Object ID (CCSDS): 27679
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.5 minutes
Inclination: 81.9766 deg
SMA: 7160.393 km
Apoapsis: 995.95 km
Periapsis: 568.566 km
RAAN: 196.2427 deg
Eccentricy: 0.02984363
Argument of periapsis: 81.8651 deg
Mean anomaly: 281.627 deg
Mean motion: 14.32839306 rev/day
Mean motion (dot): 0.0000306 rev/day2
B* drag term: 0.00067659119 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 10, 2025, 8:32 p.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 27679U 94029AEJ 25344.85563331 .00003060 00000-0 67659-3 0 9992
TLE line 2: 2 27679 81.9766 196.2427 0298436 81.8651 281.6270 14.32839306239573
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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