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.
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26883 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IUS R/B(2)
1 26883U 01033D 25241.43775759 .00000015 00000-0 00000-0 0 9991
2 26883 12.6375 18.7240 0005640 15.3116 344.7522 0.99887643 22877
Epoch: 2025-08-29T10:30Z
TLE epoch observation values (Epoch: 2025-08-29T10:30:22.255Z)
Latitude
-0.00001°
Longitude
-116.72447°
Altitude
35,871.184 km
Speed
3.072 km/s
True Right ascension
01h 15m 01s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:21:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,919.464 km
Perigee altitude
35,871.779 km
Semi-major axis
42,273.759 km
Eccentricity
0.00056
Inclination
12.6375°
RAAN
18.724°
Arg. of periapsis
15.3116°
True anomaly
344.73519°
Mean anomaly
344.7522°
Eccentric anomaly
344.7437°
Mean motion
0.24971 °/min
Orbital period
1,441.67 mins
BSTAR
0
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Other satellites on launch #33 in the year 2001 (2001-08-06 UTC)
IUS R/B(2) Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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1440 mins | 2025-08-31 12:41:48.104Z | 206.188° SW | 2025-08-31 16:44:48.104Z | 209.284° SW | 39.274° | 2025-09-01 12:41:48.104Z | 208.319° SW |
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26883 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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