STARLINK-35082, 65392
Orbit data source: Space-Track
STARLINK-35082, 65392 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sat, 30 Aug 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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65392 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-35082
1 65392U 25191P 26171.36229046 .00015325 00000-0 10638-2 0 9998
2 65392 97.3387 41.7082 0002428 94.2128 265.9377 15.05649338 45729Epoch: 2026-06-20T08:41Z
TLE epoch observation values (Epoch: 2026-06-20T08:41:41.895Z)
Latitude
-0.00004°
Longitude
2.70564°
Altitude
552.706 km
Speed
7.585 km/s
True Right ascension
02h 46m 49s
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
08:42:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.177 km
Perigee altitude
544.814 km
Semi-major axis
6,924.632 km
Eccentricity
0.00024
Inclination
97.3387°
RAAN
41.7082°
Arg. of periapsis
94.2128°
True anomaly
265.90995°
Mean anomaly
265.9377°
Eccentric anomaly
265.92382°
Mean motion
3.76659 °/min
Orbital period
95.58 mins
BSTAR
0.0010638
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Other satellites on launch #191 in the year 2025 (2025-08-30 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-35082 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 | 2026-06-21 04:24:05.755Z | 4.53° NNE | 2026-06-21 04:27:05.755Z | 280.702° WNW | 42.894° | 2026-06-21 04:30:05.755Z | 203.138° SW |
| 6 mins | 2026-06-21 15:08:05.755Z | 147.477° SSE | 2026-06-21 15:11:05.755Z | 60.14° ENE | 38.574° | 2026-06-21 15:14:05.755Z | 359.988° N |
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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