IUS R/B(1), 26882

Orbit data source: Space-Track

IUS R/B(1), 26882 is space debris in HEO 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.

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IUS R/B(1) details

Identifier	26882, 2001-033C
Orbit	HEO
Last TLE update	1 day ago
Origin	USAF SMC (US)
Manufacturer	PW CSD
Mission	Spacecraft
Bus & Motor	ORBUS 21, ORBUS 21
Mass	1,164 kg wet, 1,164 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	8.491 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 IUS R/B(1)
1 26882U 01033C   24360.02492289  .00002153  00000-0  10992-2 0  9998
2 26882  27.8639 222.8690 7098211 277.2182  13.8357  2.48939786 49061

Epoch: 2024-12-25T00:35Z

Definitive object data (Epoch: 2024-12-25T00:35:53.337Z)

Latitude	0.00034°
Longitude	119.97973°
Altitude	4,130.379 km
Speed	7.65 km/s
True Right ascension	14h 51m 54s
True Declination	0° 00' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	27.40529°
Longitude	-139.194°
Altitude	32,865.263 km
Speed	1.727 km/s
Apparent Right ascension	21h 34m 57s
Apparent Declination	19° 22' 24"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:33:09
Azimuth	359.505° N
Elevation	-30.709°
Doppler factor	1

Orbital elements

Apogee altitude	32,949.044 km
Perigee altitude	296.198 km
Semi-major axis	23,000.758 km
Eccentricity	0.7098211
Inclination	27.8639°
RAAN	222.869°
Arg. of periapsis	277.2182°
True anomaly	82.84594°
Mean anomaly	13.8357°
Eccentric anomaly	39.95113°
Mean motion	0.6222 °/min
BSTAR	0.0010992
Orbital period	578.59 mins