OBJECT CA, 55081 (Decayed)
Orbit data source: Space-Track
OBJECT CA, 55081 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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55081 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Amateur Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT CA
1 55081U 23001CA 25363.59219091 .08094748 24784-5 43075-3 0 9992
2 55081 97.3046 83.6830 0007661 279.6622 80.3813 16.42013308167478Epoch: 2025-12-29T14:12Z
TLE epoch observation values (Epoch: 2025-12-29T14:12:45.294Z)
Latitude
-0.00005°
Longitude
132.20667°
Altitude
162.876 km
Speed
7.809 km/s
True Right ascension
05h 34m 43s
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
14:31:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.26 km
Perigee altitude
152.246 km
Semi-major axis
6,535.39 km
Eccentricity
0.00077
Inclination
97.3046°
RAAN
83.683°
Arg. of periapsis
279.6622°
True anomaly
80.46787°
Mean anomaly
80.3813°
Eccentric anomaly
80.42458°
Mean motion
4.10805 °/min
Orbital period
87.63 mins
BSTAR
0.00043075
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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 CA 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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