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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 PEGASUS R/B
1 23106U 94029B 26107.05203937 .00000603 00000-0 75291-4 0 9998
2 23106 81.9554 321.0928 0111549 325.5405 33.8605 14.76530701706255Epoch: 2026-04-17T01:14Z
TLE epoch observation values (Epoch: 2026-04-17T01:14:56.201Z)
Latitude
0.00004°
Longitude
97.16786°
Altitude
578.559 km
Speed
7.606 km/s
True Right ascension
21h 24m 22s
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
01:43:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
715.605 km
Perigee altitude
559.091 km
Semi-major axis
7,015.485 km
Eccentricity
0.01115
Inclination
81.9554°
RAAN
321.0928°
Arg. of periapsis
325.5405°
True anomaly
34.58103°
Mean anomaly
33.8605°
Eccentric anomaly
34.21993°
Mean motion
3.69366 °/min
Orbital period
97.46 mins
BSTAR
0.000075291
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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 | 2026-04-18 02:13:41.434Z | 345.496° N | 2026-04-18 02:16:41.434Z | 271.855° WNW | 44.026° | 2026-04-18 02:20:41.434Z | 180.416° SSW |
| 6 mins | 2026-04-18 14:47:41.434Z | 175.46° S | 2026-04-18 14:49:41.434Z | 139.172° SSE | 42.441° | 2026-04-18 14:53:41.434Z | 13.75° 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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