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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26882 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
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
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
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)
IUS R/B(1) 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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439 mins | 2025-07-19 06:25:42.694Z | 251.707° W | 2025-07-19 06:39:42.694Z | 187.229° SSW | 33.65° | 2025-07-19 13:44:42.694Z | 176.847° S |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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