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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 PEGASUS R/B
1 23106U 94029B   26227.86886119  .00000716  00000-0  89562-4 0  9990
2 23106  81.9556 200.6763 0110212 296.7560  62.2406 14.76827376724086
Epoch: 2026-08-15T20:51Z
TLE epoch observation values (Epoch: 2026-08-15T20:51:09.606Z)
Latitude
0.00002°
Longitude
-76.38728°
Altitude
607.013 km
Speed
7.575 km/s
True Right ascension
13h 22m 42s
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
17:20:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
713.716 km
Perigee altitude
559.099 km
Semi-major axis
7,014.545 km
Eccentricity
0.01102
Inclination
81.9556°
RAAN
200.6763°
Arg. of periapsis
296.756°
True anomaly
63.36533°
Mean anomaly
62.2406°
Eccentric anomaly
62.80225°
Mean motion
3.6944 °/min
Orbital period
97.44 mins
BSTAR
0.000089562
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