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
Last TLE update
23 hours ago
Origin
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)

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TLE from 23 hours ago
0 IUS R/B(1)
1 26882U 01033C   25199.04710940  .00001213  00000-0  12912-2 0  9998
2 26882  27.8914 140.6155 7068988  51.9986 352.7708  2.49360366 54173
Epoch: 2025-07-18T01:07Z
TLE epoch observation values (Epoch: 2025-07-18T01:07:50.252Z)
Latitude
-0.00002°
Longitude
-172.48935°
Altitude
1,638.024 km
Speed
9.06 km/s
True Right ascension
09h 22m 17s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-15.95487°
Longitude
39.80211°
Altitude
29,217.237 km
Speed
2.246 km/s
Apparent Right ascension
23h 38m 24s
Apparent Declination
-19° 32' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:27:21
Azimuth
30.85° NE
Elevation
-67.078°
Doppler factor
1
Orbital elements
Apogee altitude
32,837.602 km
Perigee altitude
355.818 km
Semi-major axis
22,974.847 km
Eccentricity
0.7069
Inclination
27.8914°
RAAN
140.6155°
Arg. of periapsis
51.9986°
True anomaly
307.38389°
Mean anomaly
352.7708°
Eccentric anomaly
336.84352°
Mean motion
0.62325 °/min
Orbital period
577.61 mins
BSTAR
0.0012912
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Other satellites on launch #33 in the year 2001 (2001-08-06 UTC)
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