PEGASUS DEB, 24602

Orbit data source: Space-Track

PEGASUS DEB, 24602 is space debris in LEO originally from a launch on Thu, 19 May 1994 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
24602, 1994-029ZE
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1994-05-19 (32 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 PEGASUS DEB
1 24602U 94029ZE  26066.01325881  .00002255  00000-0  73365-3 0  9997
2 24602  81.5205 279.5895 0728942 270.6207  81.1528 13.44620016431738
Epoch: 2026-03-07T00:19Z
TLE epoch observation values (Epoch: 2026-03-07T00:19:05.561Z)
Latitude
0.00005°
Longitude
110.07533°
Altitude
1,050.473 km
Speed
7.348 km/s
True Right ascension
18h 38m 21s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:35:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,633.683 km
Perigee altitude
545.01 km
Semi-major axis
7,467.483 km
Eccentricity
0.07289
Inclination
81.5205°
RAAN
279.5895°
Arg. of periapsis
270.6207°
True anomaly
89.49411°
Mean anomaly
81.1528°
Eccentric anomaly
85.31538°
Mean motion
3.36343 °/min
Orbital period
107.03 mins
BSTAR
0.00073365
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