STARLINK-35096, 65479
Orbit data source: Space-Track
STARLINK-35096, 65479 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 03 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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65479 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-35096
1 65479U 25195X 26100.99417621 .00013654 00000-0 47244-3 0 9994
2 65479 53.1586 107.8399 0002825 73.4669 286.6642 15.30186825 34921Epoch: 2026-04-10T23:51Z
TLE epoch observation values (Epoch: 2026-04-10T23:51:36.824Z)
Latitude
-0.00002°
Longitude
-89.2834°
Altitude
475.599 km
Speed
7.63 km/s
True Right ascension
07h 11m 21s
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
20:02:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.447 km
Perigee altitude
473.575 km
Semi-major axis
6,853.648 km
Eccentricity
0.00028
Inclination
53.1586°
RAAN
107.8399°
Arg. of periapsis
73.4669°
True anomaly
286.63318°
Mean anomaly
286.6642°
Eccentric anomaly
286.64869°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
0.00047244
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Other satellites on launch #195 in the year 2025 (2025-09-03 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-35096 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 | 2026-04-12 02:40:56.620Z | 210.989° SW | 2026-04-12 02:43:56.620Z | 110.655° ESE | 38.774° | 2026-04-12 02:46:56.620Z | 58.353° ENE |
| 4 mins | 2026-04-12 04:19:56.620Z | 293.754° NW | 2026-04-12 04:21:56.620Z | 339.152° N | 21.326° | 2026-04-12 04:23:56.620Z | 19.642° NNE |
| 5 mins | 2026-04-12 09:16:56.620Z | 334.303° NNW | 2026-04-12 09:18:56.620Z | 55.826° ENE | 35.972° | 2026-04-12 09:21:56.620Z | 110.612° ESE |
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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