Key statistics
Satellite PEGASUS DEB at a glance.
Uptime
11313
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: 100.589 minutes
Inclination: 81.9808 deg
SMA: 7164.642 km
Apoapsis: 1003.219 km
Periapsis: 569.794 km
RAAN: 38.0992 deg
Eccentricy: 0.0302475
Argument of periapsis: 15.7006 deg
Mean anomaly: 345.3305 deg
Mean motion: 14.31564929 rev/day
Mean motion (dot): 0.00004848 rev/day2
B* drag term: 0.0010941 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 2:01 a.m. UTC
TLE line 0: 0 PEGASUS DEB
TLE line 1: 1 27679U 94029AEJ 25127.08415439 .00004848 00000-0 10941-2 0 9997
TLE line 2: 2 27679 81.9808 38.0992 0302475 15.7006 345.3305 14.31564929208409
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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