IUS R/B(1), 21640
Orbit data source: Space-Track
IUS R/B(1), 21640 is space debris in HEO originally from a launch on Fri, 02 Aug 1991 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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21640 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 12 hours ago
0 IUS R/B(1)
1 21640U 91054C 25214.18224066 .00008554 00000-0 16868-2 0 9998
2 21640 26.4019 207.0508 6669426 292.5918 12.2166 3.08745548330091
Epoch: 2025-08-02T04:22Z
TLE epoch observation values (Epoch: 2025-08-02T04:22:25.593Z)
Latitude
-0.00053°
Longitude
-169.57693°
Altitude
2,423.539 km
Speed
8.4 km/s
True Right ascension
13h 48m 12s
True Declination
0° 00' 02"
Sunlit
Visualization orbit readout
Latitude
22.67246°
Longitude
-47.08408°
Altitude
26,352.821 km
Speed
2.086 km/s
Apparent Right ascension
21h 29m 11s
Apparent Declination
14° 28' 35"
Sunlit
Visualization observer readout
Local Sidereal Time
06:04:53
Azimuth
307.698° NW
Elevation
-17.832°
Doppler factor
1
Orbital elements
Apogee altitude
26,837.116 km
Perigee altitude
258.316 km
Semi-major axis
19,925.853 km
Eccentricity
0.66694
Inclination
26.4019°
RAAN
207.0508°
Arg. of periapsis
292.5918°
True anomaly
67.17425°
Mean anomaly
12.2166°
Eccentric anomaly
33.06553°
Mean motion
0.77165 °/min
Orbital period
466.54 mins
BSTAR
0.0016868
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Other satellites on launch #54 in the year 1991 (1991-08-02 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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406 mins | 2025-08-03 03:51:19.138Z | 237.962° WSW | 2025-08-03 05:32:19.138Z | 160.597° S | 43.518° | 2025-08-03 10:37:19.138Z | 142.616° SSE |
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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