PEGASUS R/B, 41892
Orbit data source: Space-Track
PEGASUS R/B, 41892 is space debris in LEO originally from a launch on Thu, 15 Dec 2016 UTC launched from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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41892 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OATK FSG Utah
Mission
Spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
315 kg wet, 202 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 0.7 m
Radar Cross Section
1.381 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 PEGASUS R/B
1 41892U 16078J 26227.14658112 .00108252 00000-0 36772-3 0 9999
2 41892 34.9246 129.5716 0002533 289.2227 70.8233 15.88525666539057Epoch: 2026-08-15T03:31Z
TLE epoch observation values (Epoch: 2026-08-15T03:31:04.608Z)
Latitude
0°
Longitude
113.24076°
Altitude
304.728 km
Speed
7.728 km/s
True Right ascension
08h 38m 17s
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
09:19:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
311.465 km
Perigee altitude
308.076 km
Semi-major axis
6,687.907 km
Eccentricity
0.00025
Inclination
34.9246°
RAAN
129.5716°
Arg. of periapsis
289.2227°
True anomaly
70.85072°
Mean anomaly
70.8233°
Eccentric anomaly
70.83701°
Mean motion
3.96833 °/min
Orbital period
90.72 mins
BSTAR
0.00036772
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Other satellites on launch #78 in the year 2016 (2016-12-15 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
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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. |
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| PEGASUS R/B is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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