OBJECT M, 62620
Orbit data source: Space-Track
OBJECT M, 62620 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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62620 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational 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 day ago
TLE from 1 day ago
0 OBJECT M
1 62620U 25009M 26261.20274431 .01250193 95289-3 16076-2 0 9991
2 62620 97.3702 357.2189 0011611 272.7497 87.2456 16.07323649 94106Epoch: 2026-09-18T04:51Z
TLE epoch observation values (Epoch: 2026-09-18T04:51:57.108Z)
Latitude
-0.00003°
Longitude
-72.89806°
Altitude
257.043 km
Speed
7.753 km/s
True Right ascension
23h 48m 52s
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
02:31:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
258.741 km
Perigee altitude
243.347 km
Semi-major axis
6,629.181 km
Eccentricity
0.00116
Inclination
97.3702°
RAAN
357.2189°
Arg. of periapsis
272.7497°
True anomaly
87.37851°
Mean anomaly
87.2456°
Eccentric anomaly
87.31205°
Mean motion
4.02118 °/min
Orbital period
89.53 mins
BSTAR
0.0016076
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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. |
|---|---|---|---|---|---|---|---|
| OBJECT M is likely not visible in the next few days. |
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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