OBJECT CK, 55090 (Decayed)
Orbit data source: Space-Track
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.
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55090 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 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 16.40072436122885Epoch: 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
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
17:30:49
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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Other satellites on launch #1 in the year 2023 (2023-01-03 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 CK 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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