OBJECT AC, 47958 (Decayed)
Orbit data source: Space-Track
OBJECT AC, 47958 was a satellite in LEO that was launched on Mon, 22 Mar 2021 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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47958 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 OBJECT AC
1 47958U 21022AC 26155.97246625 .08083315 25904-5 39532-3 0 9998
2 47958 97.3573 77.8531 0009048 219.4383 140.6260 16.42190978288061Epoch: 2026-06-04T23:20Z
TLE epoch observation values (Epoch: 2026-06-04T23:20:21.083Z)
Latitude
-0.00006°
Longitude
-165.6438°
Altitude
167.812 km
Speed
7.803 km/s
True Right ascension
05h 11m 24s
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
02:14:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.696 km
Perigee altitude
150.871 km
Semi-major axis
6,534.92 km
Eccentricity
0.0009
Inclination
97.3573°
RAAN
77.8531°
Arg. of periapsis
219.4383°
True anomaly
140.69172°
Mean anomaly
140.626°
Eccentric anomaly
140.65886°
Mean motion
4.10849 °/min
Orbital period
87.62 mins
BSTAR
0.00039532
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Other satellites on launch #22 in the year 2021 (2021-03-22 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT AC Visibility
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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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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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