IUS R/B(2), 21641

Orbit data source: Space-Track

IUS R/B(2), 21641 is space debris in GEO originally from a launch on Fri, 02 Aug 1991 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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Identifier
21641, 1991-054D
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 6, Unknown motor
Mass
~1,100 kg wet, ~1,100 kg dry
Launch date (UTC)
1991-08-02 (34 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
8.086 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 IUS R/B(2)
1 21641U 91054D   25348.53702831 -.00000086  00000-0  00000-0 0  9999
2 21641  13.9566 334.4614 0036508 340.6981 210.8517  1.00390081 45515
Epoch: 2025-12-14T12:53Z
TLE epoch observation values (Epoch: 2025-12-14T12:53:19.245Z)
Latitude
-2.72794°
Longitude
-111.31163°
Altitude
35,885 km
Speed
3.066 km/s
True Right ascension
11h 01m 52s
True Declination
-2° 43' 31"
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
13:23:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,908.262 km
Perigee altitude
35,600.627 km
Semi-major axis
42,132.582 km
Eccentricity
0.00365
Inclination
13.9566°
RAAN
334.4614°
Arg. of periapsis
340.6981°
True anomaly
210.638°
Mean anomaly
210.8517°
Eccentric anomaly
210.74477°
Mean motion
0.25097 °/min
Orbital period
1,434.45 mins
BSTAR
0
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Other satellites on launch #54 in the year 1991 (1991-08-02 UTC)

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