OBJECT AD, 47959 (Decayed)
Orbit data source: Space-Track
OBJECT AD, 47959 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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47959 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT AD
1 47959U 21022AD 25160.45426279 .07940347 25506-5 90589-3 0 9995
2 47959 97.3899 75.6235 0011032 227.2558 132.7812 16.36806138232695Epoch: 2025-06-09T10:54Z
TLE epoch observation values (Epoch: 2025-06-09T10:54:08.305Z)
Latitude
-0.00001°
Longitude
14.02365°
Altitude
182.475 km
Speed
7.794 km/s
True Right ascension
05h 02m 29s
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
23:54:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
178.349 km
Perigee altitude
163.899 km
Semi-major axis
6,549.261 km
Eccentricity
0.0011
Inclination
97.3899°
RAAN
75.6235°
Arg. of periapsis
227.2558°
True anomaly
132.8739°
Mean anomaly
132.7812°
Eccentric anomaly
132.82756°
Mean motion
4.09501 °/min
Orbital period
87.91 mins
BSTAR
0.00090589
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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 AD 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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