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: 5 hours ago

TLE from 5 hours ago
0 PEGASUS R/B
1 23106U 94029B   26062.79842618  .00001994  00000-0  25486-3 0  9998
2 23106  81.9593   5.1689 0113887 106.9476 254.4255 14.76382659699720
Epoch: 2026-03-03T19:09Z
TLE epoch observation values (Epoch: 2026-03-03T19:09:44.021Z)
Latitude
-0°
Longitude
-83.83684°
Altitude
666.087 km
Speed
7.512 km/s
True Right ascension
00h 20m 40s
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
04:08:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
717.72 km
Perigee altitude
557.914 km
Semi-major axis
7,015.954 km
Eccentricity
0.01139
Inclination
81.9593°
RAAN
5.1689°
Arg. of periapsis
106.9476°
True anomaly
253.17326°
Mean anomaly
254.4255°
Eccentric anomaly
253.79889°
Mean motion
3.69329 °/min
Orbital period
97.47 mins
BSTAR
0.00025486
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