OBJECT M, 63221
Orbit data source: Space-Track
OBJECT M, 63221 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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63221 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Defense Calibration
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 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 63221U 25052M 26259.51286003 .00003226 00000-0 14232-3 0 9995
2 63221 97.3735 150.0045 0003813 153.3512 206.7921 15.22475662 83738Epoch: 2026-09-16T12:18Z
TLE epoch observation values (Epoch: 2026-09-16T12:18:31.106Z)
Latitude
-0.00005°
Longitude
-30.08848°
Altitude
503.812 km
Speed
7.611 km/s
True Right ascension
10h 00m 01s
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
06:18:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.958 km
Perigee altitude
492.716 km
Semi-major axis
6,873.474 km
Eccentricity
0.00038
Inclination
97.3735°
RAAN
150.0045°
Arg. of periapsis
153.3512°
True anomaly
206.77241°
Mean anomaly
206.7921°
Eccentric anomaly
206.78226°
Mean motion
3.80872 °/min
Orbital period
94.52 mins
BSTAR
0.00014232
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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 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 | 2026-09-17 16:49:23.390Z | 165.835° S | 2026-09-17 16:52:23.390Z | 154.561° SSE | 75.839° | 2026-09-17 16:55:23.390Z | 349.096° N |
| 6 mins | 2026-09-18 05:53:23.390Z | 359.895° N | 2026-09-18 05:55:23.390Z | 318.338° NNW | 55.355° | 2026-09-18 05:59:23.390Z | 204.445° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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