STARLINK-35122, 65510
Orbit data source: Space-Track
STARLINK-35122, 65510 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 05 Sep 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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65510 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-35122
1 65510U 25198U 26171.35290644 .00015311 00000-0 46358-3 0 9992
2 65510 53.1588 152.3369 0001442 80.9217 279.1949 15.34385551 44364Epoch: 2026-06-20T08:28Z
TLE epoch observation values (Epoch: 2026-06-20T08:28:11.116Z)
Latitude
0.00001°
Longitude
116.72184°
Altitude
463.49 km
Speed
7.636 km/s
True Right ascension
10h 09m 20s
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
07:15:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.99 km
Perigee altitude
462.017 km
Semi-major axis
6,841.14 km
Eccentricity
0.00014
Inclination
53.1588°
RAAN
152.3369°
Arg. of periapsis
80.9217°
True anomaly
279.17859°
Mean anomaly
279.1949°
Eccentric anomaly
279.18674°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
0.00046358
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Other satellites on launch #198 in the year 2025 (2025-09-05 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.STARLINK-35122 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 | 2026-06-21 00:15:25.178Z | 161.102° S | 2026-06-21 00:17:25.178Z | 125.057° SE | 14.946° | 2026-06-21 00:19:25.178Z | 90.574° ESE |
| 5 mins | 2026-06-21 01:52:25.178Z | 249.209° W | 2026-06-21 01:54:25.178Z | 308.947° NW | 40.036° | 2026-06-21 01:57:25.178Z | 40.78° NE |
| 5 mins | 2026-06-21 08:26:25.178Z | 302.547° NW | 2026-06-21 08:28:25.178Z | 234.611° WSW | 43.451° | 2026-06-21 08:31:25.178Z | 139.316° SSE |
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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