OBJECT CN, 62693
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, 62693 is 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.
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62693 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational 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: 4 days ago
TLE from 4 days ago
0 OBJECT CN
1 62693U 25009CN 25309.68627329 .00056820 00000-0 15235-2 0 9993
2 62693 97.4330 31.2306 0001563 274.3700 85.7366 15.37782828102613Epoch: 2025-11-05T16:28Z
TLE epoch observation values (Epoch: 2025-11-05T16:28:14.012Z)
Latitude
-0.00001°
Longitude
99.01684°
Altitude
455.702 km
Speed
7.639 km/s
True Right ascension
02h 04m 55s
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
02:58:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.678 km
Perigee altitude
448.543 km
Semi-major axis
6,827.748 km
Eccentricity
0.00016
Inclination
97.433°
RAAN
31.2306°
Arg. of periapsis
274.37°
True anomaly
85.75446°
Mean anomaly
85.7366°
Eccentric anomaly
85.74553°
Mean motion
3.84704 °/min
Orbital period
93.58 mins
BSTAR
0.0015235
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-09 17:51:07.510Z | 43.059° NE | 2025-11-09 17:53:07.510Z | 84.167° E | 23.025° | 2025-11-09 17:56:07.510Z | 152.606° SSE |
| 4 mins | 2025-11-10 05:55:07.510Z | 198.617° SSW | 2025-11-10 05:56:07.510Z | 230.501° WSW | 35.751° | 2025-11-10 05:59:07.510Z | 333.234° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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