Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11435
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: 100.548 minutes
Inclination: 81.9772 deg
SMA: 7162.685 km
Apoapsis: 999.292 km
Periapsis: 569.808 km
RAAN: 288.4977 deg
Eccentricy: 0.02998062
Argument of periapsis: 20.8606 deg
Mean anomaly: 340.451 deg
Mean motion: 14.32151565 rev/day
Mean motion (dot): 0.00005145 rev/day2
B* drag term: 0.0011556093 1/REarth
Two-line elements (TLE)
Creation date: Sept. 2, 2025, 11:42 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 9:24 a.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 27679U 94029AEJ 25245.39223002 .00005145 00000-0 11556-2 0 9999
TLE line 2: 2 27679 81.9772 288.4977 0299806 20.8606 340.4510 14.32151565225333
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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