OBJECT CN, 51068 (Decayed)
Orbit data source: Space-Track
OBJECT CN, 51068 was a satellite in LEO that was launched on Thu, 13 Jan 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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51068 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Radar Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT CN
1 51068U 22002CN 26087.87218396 .02787700 23919-5 10450-2 0 9995
2 51068 97.2857 173.5980 0010179 256.9690 103.0466 16.24296805234763Epoch: 2026-03-28T20:55Z
TLE epoch observation values (Epoch: 2026-03-28T20:55:56.694Z)
Latitude
0.00008°
Longitude
33.32557°
Altitude
212.665 km
Speed
7.778 km/s
True Right ascension
11h 34m 23s
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
22:52:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
211.435 km
Perigee altitude
198.034 km
Semi-major axis
6,582.871 km
Eccentricity
0.00102
Inclination
97.2857°
RAAN
173.598°
Arg. of periapsis
256.969°
True anomaly
103.1602°
Mean anomaly
103.0466°
Eccentric anomaly
103.1034°
Mean motion
4.06369 °/min
Orbital period
88.59 mins
BSTAR
0.001045
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Other satellites on launch #2 in the year 2022 (2022-01-13 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 CN 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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