OBJECT Y, 63232
Orbit data source: Space-Track
OBJECT Y, 63232 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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63232 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Astro Digital
Mission
Operational Commercial Technology
Bus & Motor
CORVUS-MICRO, Unknown motor
Mass
32 kg wet, 32 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.400 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT Y
1 63232U 25052Y 26260.42412990 .00005047 00000-0 20569-3 0 9998
2 63232 97.3803 152.1448 0005787 165.8585 194.2816 15.24896237 83928Epoch: 2026-09-17T10:10Z
TLE epoch observation values (Epoch: 2026-09-17T10:10:44.823Z)
Latitude
-0.00001°
Longitude
3.09647°
Altitude
498.048 km
Speed
7.613 km/s
True Right ascension
10h 08m 34s
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
12:07:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.029 km
Perigee altitude
484.082 km
Semi-major axis
6,866.192 km
Eccentricity
0.00058
Inclination
97.3803°
RAAN
152.1448°
Arg. of periapsis
165.8585°
True anomaly
194.26525°
Mean anomaly
194.2816°
Eccentric anomaly
194.27343°
Mean motion
3.81478 °/min
Orbital period
94.37 mins
BSTAR
0.00020569
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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 Y 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 | 2026-09-18 05:38:34.710Z | 17.729° NNE | 2026-09-18 05:41:34.710Z | 129.678° SE | 69.865° | 2026-09-18 05:44:34.710Z | 185.75° SSW |
| 4 mins | 2026-09-18 16:15:34.710Z | 109.938° ESE | 2026-09-18 16:17:34.710Z | 60.797° ENE | 24.622° | 2026-09-18 16:19:34.710Z | 21.433° NNE |
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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