OBJECT M, 62620
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 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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Edit Public Description
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, 0.2 m
Radar Cross Section
0.121 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OBJECT M
1 62620U 25009M 25345.22595378 .00059945 00000-0 16384-2 0 9998
2 62620 97.4125 65.7234 0003615 251.7169 108.3683 15.37169308 50376Epoch: 2025-12-11T05:25Z
TLE epoch observation values (Epoch: 2025-12-11T05:25:22.406Z)
Latitude
0.00005°
Longitude
-95.80494°
Altitude
458.377 km
Speed
7.637 km/s
True Right ascension
04h 22m 53s
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
16:50:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.897 km
Perigee altitude
448.959 km
Semi-major axis
6,829.565 km
Eccentricity
0.00036
Inclination
97.4125°
RAAN
65.7234°
Arg. of periapsis
251.7169°
True anomaly
108.40761°
Mean anomaly
108.3683°
Eccentric anomaly
108.38795°
Mean motion
3.84551 °/min
Orbital period
93.62 mins
BSTAR
0.0016384
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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 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-11 18:28:13.206Z | 9.277° NNE | 2025-12-11 18:31:13.206Z | 345.22° N | 42.64° | 2025-12-11 18:34:13.206Z | 197.663° SSW |
| 4 mins | 2025-12-12 05:01:13.206Z | 105.303° ESE | 2025-12-12 05:02:13.206Z | 76.184° E | 24.742° | 2025-12-12 05:05:13.206Z | 12.647° NNE |
| 4 mins | 2025-12-12 17:56:13.206Z | 48.993° ENE | 2025-12-12 17:58:13.206Z | 111.122° ESE | 27.367° | 2025-12-12 18:00:13.206Z | 156.324° SSE |
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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