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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23106 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OSC Chandler
Mission
Spacecraft
Bus & Motor
HAPS, Unknown motor
Mass
107 kg wet, 97 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.4 m
Radar Cross Section
0.286 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 PEGASUS R/B
1 23106U 94029B 26175.22273412 .00001212 00000-0 15245-3 0 9996
2 23106 81.9560 253.1505 0113276 105.6373 255.7371 14.76712121716319Epoch: 2026-06-24T05:20Z
TLE epoch observation values (Epoch: 2026-06-24T05:20:44.227Z)
Latitude
-0.00006°
Longitude
-99.41683°
Altitude
663.167 km
Speed
7.515 km/s
True Right ascension
16h 52m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:06:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
716.235 km
Perigee altitude
557.311 km
Semi-major axis
7,014.91 km
Eccentricity
0.01133
Inclination
81.956°
RAAN
253.1505°
Arg. of periapsis
105.6373°
True anomaly
254.48354°
Mean anomaly
255.7371°
Eccentric anomaly
255.10987°
Mean motion
3.69411 °/min
Orbital period
97.45 mins
BSTAR
0.00015245
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Other satellites on launch #29 in the year 1994 (1994-05-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.PEGASUS R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-24 17:17:42.859Z | 345.929° N | 2026-06-24 17:20:42.859Z | 302.468° NW | 42.44° | 2026-06-24 17:24:42.859Z | 181.001° SSW |
| 6 mins | 2026-06-25 05:52:42.859Z | 177.376° S | 2026-06-25 05:54:42.859Z | 146.782° SSE | 42.43° | 2026-06-25 05:58:42.859Z | 12.938° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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