DECAYED

OBJECT CK, 55090 (Decayed)

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 CK, 55090 was a satellite in LEO that was launched on Tue, 03 Jan 2023 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.

Not visible in the next 10 days
Identifier
55090, 2023-001CK
Orbit
Decayed
Country
Flag of TBDTBD
Related business
Manufacturer
EPICU
Mission
Decayed Commercial Technology
Bus & Motor
CHIMERA, AOCS
Mass
270 kg wet, 100 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Unknown
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.625 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 months ago

TLE from 7 months ago
0 OBJECT CK
1 55090U 23001CK  25074.25110233  .11585656  25205-5  84256-3 0  9994
2 55090  97.3487 151.4600 0012027 264.7101  95.2826 16.40072436122885
Epoch: 2025-03-15T06:01Z
TLE epoch observation values (Epoch: 2025-03-15T06:01:35.241Z)
Latitude
-0.00005°
Longitude
-112.03616°
Altitude
169.597 km
Speed
7.804 km/s
True Right ascension
10h 05m 50s
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
19:27:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170.281 km
Perigee altitude
154.549 km
Semi-major axis
6,540.552 km
Eccentricity
0.0012
Inclination
97.3487°
RAAN
151.46°
Arg. of periapsis
264.7101°
True anomaly
95.41981°
Mean anomaly
95.2826°
Eccentric anomaly
95.35121°
Mean motion
4.10319 °/min
Orbital period
87.74 mins
BSTAR
0.00084256
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