OBJECT Q, 47946 (Decayed)
Orbit data source: Space-Track
OBJECT Q, 47946 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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47946 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 OBJECT Q
1 47946U 21022Q 25316.72238787 .11822108 26497-5 96220-3 0 9996
2 47946 97.3833 235.5563 0007164 145.3688 214.8079 16.39929835258042Epoch: 2025-11-12T17:20Z
TLE epoch observation values (Epoch: 2025-11-12T17:20:14.311Z)
Latitude
-0.00008°
Longitude
-76.59383°
Altitude
173.092 km
Speed
7.8 km/s
True Right ascension
15h 42m 13s
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
19:31:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.482 km
Perigee altitude
158.11 km
Semi-major axis
6,540.933 km
Eccentricity
0.00072
Inclination
97.3833°
RAAN
235.5563°
Arg. of periapsis
145.3688°
True anomaly
214.76107°
Mean anomaly
214.8079°
Eccentric anomaly
214.78448°
Mean motion
4.10283 °/min
Orbital period
87.74 mins
BSTAR
0.0009622
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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 Q 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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