IABS R/B, 22916

Orbit data source: Space-Track

IABS R/B, 22916 is space debris in GEO originally from a launch on Sun, 28 Nov 1993 UTC launched from the Air Force Eastern Test Range (AFETR). 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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IABS R/B details

Identifier	22916, 1993-074B
Orbit	GEO
Last TLE update	1 day ago
Origin	USAF SMC (US)
Manufacturer	MM/Valley Forge
Mission	Spacecraft
Bus & Motor	R-4D, R-4D-12 X2
Mass	270 kg wet, 270 kg dry
Launch date (UTC)	1993-11-28 (31 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 2.9 m
Radar Cross Section	4.851 m²

Expand to show TLE details & history

TLE from 1 day ago

0 IABS R/B
1 22916U 93074B   25034.94084442  .00000051  00000-0  00000-0 0  9998
2 22916  14.1378 345.7443 0063856  93.7701 266.9863  0.99976951 20929

Epoch: 2025-02-03T22:34Z

Definitive object data (Epoch: 2025-02-03T22:34:48.957Z)

Latitude	0.00001°
Longitude	-127.27874°
Altitude	35,885.89 km
Speed	3.07 km/s
True Right ascension	23h 03m 06s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	13.99569°
Longitude	-45.9812°
Altitude	35,605.143 km
Speed	3.091 km/s
Apparent Right ascension	04h 16m 08s
Apparent Declination	9° 30' 04"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	06:00:52
Azimuth	224.603° SW
Elevation	51.697°
Doppler factor	1

Orbital elements

Apogee altitude	36,140.208 km
Perigee altitude	35,600.643 km
Semi-major axis	42,248.563 km
Eccentricity	0.0063856
Inclination	14.1378°
RAAN	345.7443°
Arg. of periapsis	93.7701°
True anomaly	266.2559°
Mean anomaly	266.9863°
Eccentric anomaly	266.62107°
Mean motion	0.24993 °/min
BSTAR	Unknown
Orbital period	1440.38 mins