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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Identifier
41892, 2016-078J
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OATK FSG Utah
Mission
Spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
315 kg wet, 202 kg dry
Launch date (UTC)
2016-12-15 (9 years ago)
Launch vehicle
Unknown
Launch site
Pegasus Launch, Eastern Range Air Space (ERAS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 0.7 m
Radar Cross Section
1.381 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 PEGASUS R/B
1 41892U 16078J   26034.11745229  .00048290  00000-0  53864-3 0  9994
2 41892  34.9346   0.2456 0005563 355.1387   4.9284 15.61665532508632
Epoch: 2026-02-03T02:49Z
TLE epoch observation values (Epoch: 2026-02-03T02:49:07.877Z)
Latitude
-0.00002°
Longitude
-175.34024°
Altitude
377.981 km
Speed
7.688 km/s
True Right ascension
00h 00m 58s
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
09:47:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
389.924 km
Perigee altitude
382.398 km
Semi-major axis
6,764.298 km
Eccentricity
0.00056
Inclination
34.9346°
RAAN
0.2456°
Arg. of periapsis
355.1387°
True anomaly
4.93388°
Mean anomaly
4.9284°
Eccentric anomaly
4.93114°
Mean motion
3.9013 °/min
Orbital period
92.28 mins
BSTAR
0.00053864
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