OBJECT M, 62620 (Decayed)
Orbit data source: Space-Track
OBJECT M, 62620 was a satellite in LEO 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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62620 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Defense Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.4 m
Radar Cross Section
0.121 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 OBJECT M
1 62620U 25009M 26266.39787560 .14868253 25513-5 37179-3 0 9997
2 62620 97.3605 3.0838 0015262 274.1298 85.8260 16.44649019 94948Epoch: 2026-09-23T09:32Z
TLE epoch observation values (Epoch: 2026-09-23T09:32:56.451Z)
Latitude
-0°
Longitude
-142.40099°
Altitude
156.013 km
Speed
7.813 km/s
True Right ascension
00h 12m 20s
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
17:14:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.228 km
Perigee altitude
140.301 km
Semi-major axis
6,528.401 km
Eccentricity
0.00153
Inclination
97.3605°
RAAN
3.0838°
Arg. of periapsis
274.1298°
True anomaly
86.00045°
Mean anomaly
85.826°
Eccentric anomaly
85.91322°
Mean motion
4.11465 °/min
Orbital period
87.49 mins
BSTAR
0.00037179
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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 M 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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