PEGASUS R/B, 23106

Orbit data source: Space-Track

PEGASUS R/B, 23106 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
23106, 1994-029B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OSC Chandler
Mission
Spacecraft
Bus & Motor
HAPS, Unknown motor
Mass
107 kg wet, 97 kg dry
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
Cyl, 0.4 m
Radar Cross Section
0.286 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 PEGASUS R/B
1 23106U 94029B   26119.58882109  .00001101  00000-0  13993-3 0  9997
2 23106  81.9540 308.5970 0110924 284.8353  74.0591 14.76551622708104
Epoch: 2026-04-29T14:07Z
TLE epoch observation values (Epoch: 2026-04-29T14:07:54.142Z)
Latitude
0.00005°
Longitude
-120.9262°
Altitude
622.659 km
Speed
7.558 km/s
True Right ascension
20h 34m 23s
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
09:28:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
715.1 km
Perigee altitude
559.464 km
Semi-major axis
7,015.419 km
Eccentricity
0.01109
Inclination
81.954°
RAAN
308.597°
Arg. of periapsis
284.8353°
True anomaly
75.28589°
Mean anomaly
74.0591°
Eccentric anomaly
74.67204°
Mean motion
3.69371 °/min
Orbital period
97.46 mins
BSTAR
0.00013993
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