IUS R/B(2), 26883

Orbit data source: Space-Track

IUS R/B(2), 26883 is space debris in GEO originally from a launch on Mon, 06 Aug 2001 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.

Loading next visibility...

IUS R/B(2) details

Identifier	26883, 2001-033D
Orbit	GEO
Last TLE update	1 day ago
Origin	USAF SMC (US)
Manufacturer	PW CSD
Mission	Orbus 6E) (Titan IVB IUS)"
Bus & Motor	ORBUS 6, ORBUS 6
Mass	1,079 kg wet, 1,079 kg dry
Launch date (UTC)	2001-08-06 (23 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, Unknown HBR
Radar Cross Section	8.086 m²

Expand to show TLE details & history

TLE from 1 day ago

0 IUS R/B(2)
1 26883U 01033D   24360.18843055  .00000115  00000-0  00000-0 0  9990
2 26883  12.3965  20.3631 0005507   9.3274 350.6831  0.99892756 20409

Epoch: 2024-12-25T04:31Z

Definitive object data (Epoch: 2024-12-25T04:31:20.399Z)

Latitude	0.00001°
Longitude	-141.6637°
Altitude	35,869.82 km
Speed	3.072 km/s
True Right ascension	01h 21m 25s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	12.42174°
Longitude	-51.62241°
Altitude	35,888.071 km
Speed	3.071 km/s
Apparent Right ascension	07h 03m 05s
Apparent Declination	7° 36' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:54:18
Azimuth	241.534° WSW
Elevation	39.992°
Doppler factor	1

Orbital elements

Apogee altitude	35,917.462 km
Perigee altitude	35,870.903 km
Semi-major axis	42,272.319 km
Eccentricity	0.0005507
Inclination	12.3965°
RAAN	20.3631°
Arg. of periapsis	9.3274°
True anomaly	350.67288°
Mean anomaly	350.6831°
Eccentric anomaly	350.67799°
Mean motion	0.24972 °/min
BSTAR	Unknown
Orbital period	1441.6 mins