OBJECT J, 63218
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 J, 63218 is a satellite in SSO that was launched on Sat, 15 Mar 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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63218 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT J
1 63218U 25052J 25317.13055403 .00034057 00000-0 13523-2 0 9998
2 63218 97.4083 209.0153 0003873 135.8736 224.2812 15.25251467 37062Epoch: 2025-11-13T03:07Z
TLE epoch observation values (Epoch: 2025-11-13T03:07:59.868Z)
Latitude
0.00004°
Longitude
109.52303°
Altitude
495.033 km
Speed
7.616 km/s
True Right ascension
13h 56m 03s
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
00:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.648 km
Perigee altitude
484.33 km
Semi-major axis
6,865.126 km
Eccentricity
0.00039
Inclination
97.4083°
RAAN
209.0153°
Arg. of periapsis
135.8736°
True anomaly
224.25022°
Mean anomaly
224.2812°
Eccentric anomaly
224.26571°
Mean motion
3.81567 °/min
Orbital period
94.35 mins
BSTAR
0.0013523
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Other satellites on launch #52 in the year 2025 (2025-03-15 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 J 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 | 2025-11-15 06:04:50.677Z | 357.631° N | 2025-11-15 06:07:50.677Z | 252.834° W | 36.764° | 2025-11-15 06:09:50.677Z | 212.502° SW |
| 5 mins | 2025-11-15 16:40:50.677Z | 140.829° SSE | 2025-11-15 16:42:50.677Z | 80.859° E | 36.74° | 2025-11-15 16:45:50.677Z | 2.317° NNE |
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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