PEGASUS DEB, 39308

Orbit data source: Space-Track

PEGASUS DEB, 39308 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
39308, 1994-029AET
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: 3 days ago

TLE from 3 days ago
0 PEGASUS DEB
1 39308U 94029AET 26171.33473075  .00003928  00000-0  71377-3 0  9996
2 39308  81.9660  18.9702 0340282  15.8958 345.2593 14.34680280681177
Epoch: 2026-06-20T08:02Z
TLE epoch observation values (Epoch: 2026-06-20T08:02:00.736Z)
Latitude
-0.00005°
Longitude
-10.08371°
Altitude
544.168 km
Speed
7.714 km/s
True Right ascension
01h 15m 52s
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
07:07:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,016.58 km
Perigee altitude
529.883 km
Semi-major axis
7,151.369 km
Eccentricity
0.03403
Inclination
81.966°
RAAN
18.9702°
Arg. of periapsis
15.8958°
True anomaly
344.2247°
Mean anomaly
345.2593°
Eccentric anomaly
344.74636°
Mean motion
3.58888 °/min
Orbital period
100.31 mins
BSTAR
0.00071377
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