OBJECT CN, 51068

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT CN, 51068 is a satellite in SSO 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.

Not visible in the next 10 days
Identifier
51068, 2022-002CN
Orbit
SSO
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Commercial Radar Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2022-01-13 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 OBJECT CN
1 51068U 22002CN  26070.45874509  .00466381  87607-4  13253-2 0  9999
2 51068  97.2916 154.5314 0004678 253.1627 106.9135 15.93315490231977
Epoch: 2026-03-11T11:00Z
TLE epoch observation values (Epoch: 2026-03-11T11:00:35.575Z)
Latitude
-0.00004°
Longitude
-179.73951°
Altitude
297.114 km
Speed
7.729 km/s
True Right ascension
10h 18m 07s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
09:22:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
292.995 km
Perigee altitude
286.757 km
Semi-major axis
6,668.013 km
Eccentricity
0.00047
Inclination
97.2916°
RAAN
154.5314°
Arg. of periapsis
253.1627°
True anomaly
106.96478°
Mean anomaly
106.9135°
Eccentric anomaly
106.93914°
Mean motion
3.9861 °/min
Orbital period
90.31 mins
BSTAR
0.0013253
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Computing Atmospheric mass density...

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