STARLINK-35265, 65748
Orbit data source: Space-Track
STARLINK-35265, 65748 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 25 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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65748 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-35265
1 65748U 25216Q 26171.43585022 .00009509 00000-0 33267-3 0 9999
2 65748 53.1582 215.7061 0001140 87.5135 272.5996 15.30209315 41197Epoch: 2026-06-20T10:27Z
TLE epoch observation values (Epoch: 2026-06-20T10:27:37.459Z)
Latitude
-0.00007°
Longitude
150.14947°
Altitude
476.051 km
Speed
7.629 km/s
True Right ascension
14h 22m 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
07:12:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.225 km
Perigee altitude
474.663 km
Semi-major axis
6,853.581 km
Eccentricity
0.00011
Inclination
53.1582°
RAAN
215.7061°
Arg. of periapsis
87.5135°
True anomaly
272.58655°
Mean anomaly
272.5996°
Eccentric anomaly
272.59307°
Mean motion
3.82531 °/min
Orbital period
94.11 mins
BSTAR
0.00033267
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Other satellites on launch #216 in the year 2025 (2025-09-25 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-35265 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 05:26:36.895Z | 216.017° SW | 2026-06-21 05:29:36.895Z | 127.184° SE | 41.661° | 2026-06-21 05:32:36.895Z | 57.098° ENE |
| 5 mins | 2026-06-21 12:02:36.895Z | 328.017° NNW | 2026-06-21 12:04:36.895Z | 41.67° NE | 38.698° | 2026-06-21 12:07:36.895Z | 112.531° SE |
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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