OBJECT DM, 63002 (Decayed)
Orbit data source: Space-Track
OBJECT DM, 63002 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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63002 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 OBJECT DM
1 63002U 25009DM 26120.63486468 .15714382 25502-5 56124-3 0 9994
2 63002 97.3806 214.5358 0013850 275.5212 84.4509 16.42995914130021Epoch: 2026-04-30T15:14Z
TLE epoch observation values (Epoch: 2026-04-30T15:14:12.308Z)
Latitude
-0.00004°
Longitude
127.40587°
Altitude
160.238 km
Speed
7.81 km/s
True Right ascension
14h 18m 08s
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
22:16:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.696 km
Perigee altitude
145.6 km
Semi-major axis
6,532.785 km
Eccentricity
0.00139
Inclination
97.3806°
RAAN
214.5358°
Arg. of periapsis
275.5212°
True anomaly
84.60889°
Mean anomaly
84.4509°
Eccentric anomaly
84.52989°
Mean motion
4.11051 °/min
Orbital period
87.58 mins
BSTAR
0.00056124
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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 DM 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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