PEGASUS DEB, 39306

Orbit data source: Space-Track

PEGASUS DEB, 39306 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
39306, 1994-029AER
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: 1 week ago

TLE from 1 week ago
0 PEGASUS DEB
1 39306U 94029AER 26057.27733312  .00074995  00000-0  46128-2 0  9990
2 39306  81.7323 356.2383 0122741  77.7128 283.7806 15.03561005 92186
Epoch: 2026-02-26T06:39Z
TLE epoch observation values (Epoch: 2026-02-26T06:39:21.581Z)
Latitude
-0.00007°
Longitude
100.2679°
Altitude
539.681 km
Speed
7.603 km/s
True Right ascension
23h 44m 57s
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
14:34:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.025 km
Perigee altitude
467.879 km
Semi-major axis
6,931.089 km
Eccentricity
0.01227
Inclination
81.7323°
RAAN
356.2383°
Arg. of periapsis
77.7128°
True anomaly
282.4097°
Mean anomaly
283.7806°
Eccentric anomaly
283.09564°
Mean motion
3.76133 °/min
Orbital period
95.71 mins
BSTAR
0.0046128
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