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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Identifier
26882, 2001-033C
Orbit
HEO
Country
Flag of USUS
Related business
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 (24 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
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 IUS R/B(1)
1 26882U 01033C   25259.16830242  .00003435  00000-0  22196-2 0  9999
2 26882  27.8839 116.0855 7089319  91.9362 343.1234  2.49605264 55679
Epoch: 2025-09-16T04:02Z
TLE epoch observation values (Epoch: 2025-09-16T04:02:21.329Z)
Latitude
-0.00007°
Longitude
60.24036°
Altitude
5,281.094 km
Speed
7.142 km/s
True Right ascension
07h 44m 46s
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
03:44:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,858.691 km
Perigee altitude
304.744 km
Semi-major axis
22,959.855 km
Eccentricity
0.70893
Inclination
27.8839°
RAAN
116.0855°
Arg. of periapsis
91.9362°
True anomaly
268.12831°
Mean anomaly
343.1234°
Eccentric anomaly
313.81249°
Mean motion
0.62386 °/min
Orbital period
577.05 mins
BSTAR
0.0022196
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Other satellites on launch #33 in the year 2001 (2001-08-06 UTC)

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