OBJECT CN, 62693 (Decayed)
Orbit data source: Space-Track
OBJECT CN, 62693 was a satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62693 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.014 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT CN
1 62693U 25009CN 26125.99287441 .02271390 57702-2 23247-2 0 9999
2 62693 97.3937 219.8957 0014907 270.4030 89.5546 16.12023424130831Epoch: 2026-05-05T23:49Z
TLE epoch observation values (Epoch: 2026-05-05T23:49:44.349Z)
Latitude
-0.00003°
Longitude
-1.39884°
Altitude
244.451 km
Speed
7.76 km/s
True Right ascension
14h 39m 34s
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
07:22:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
248.005 km
Perigee altitude
228.279 km
Semi-major axis
6,616.279 km
Eccentricity
0.00149
Inclination
97.3937°
RAAN
219.8957°
Arg. of periapsis
270.403°
True anomaly
89.72542°
Mean anomaly
89.5546°
Eccentric anomaly
89.64001°
Mean motion
4.03295 °/min
Orbital period
89.26 mins
BSTAR
0.0023247
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Other satellites on launch #9 in the year 2025 (2025-01-14 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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