OBJECT AY, 62655
Orbit data source: Space-Track
OBJECT AY, 62655 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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62655 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Navigation
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.480 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 AY
1 62655U 25009AY 26215.77100050 .00027103 00000-0 60090-3 0 9997
2 62655 97.4014 302.9367 0002722 111.3657 248.7882 15.43719325 86539Epoch: 2026-08-03T18:30Z
TLE epoch observation values (Epoch: 2026-08-03T18:30:14.443Z)
Latitude
0.00003°
Longitude
73.02719°
Altitude
438.938 km
Speed
7.648 km/s
True Right ascension
20h 11m 44s
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
17:49:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.932 km
Perigee altitude
430.224 km
Semi-major axis
6,810.215 km
Eccentricity
0.00027
Inclination
97.4014°
RAAN
302.9367°
Arg. of periapsis
111.3657°
True anomaly
248.75913°
Mean anomaly
248.7882°
Eccentric anomaly
248.77366°
Mean motion
3.86191 °/min
Orbital period
93.22 mins
BSTAR
0.0006009
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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 AY 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-05 06:26:01.646Z | 222.026° SW | 2026-08-05 06:27:01.646Z | 254.5° W | 27.428° | 2026-08-05 06:30:01.646Z | 325.984° NNW |
| 4 mins | 2026-08-05 19:18:01.646Z | 331.831° NNW | 2026-08-05 19:19:01.646Z | 305.123° NW | 25.278° | 2026-08-05 19:22:01.646Z | 228.584° WSW |
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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