STARLINK-35251, 65604
Orbit data source: Space-Track
STARLINK-35251, 65604 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sat, 13 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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65604 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: 1 day ago
TLE from 1 day ago
0 STARLINK-35251
1 65604U 25207N 26166.13678309 .00004116 00000-0 28895-3 0 9992
2 65604 97.3566 233.7895 0000748 90.5606 269.5707 15.05662145 42929Epoch: 2026-06-15T03:16Z
TLE epoch observation values (Epoch: 2026-06-15T03:16:58.058Z)
Latitude
-0.00007°
Longitude
-78.87989°
Altitude
552.55 km
Speed
7.585 km/s
True Right ascension
15h 35m 09s
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
13:36:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.975 km
Perigee altitude
545.939 km
Semi-major axis
6,924.594 km
Eccentricity
0.00007
Inclination
97.3566°
RAAN
233.7895°
Arg. of periapsis
90.5606°
True anomaly
269.56213°
Mean anomaly
269.5707°
Eccentric anomaly
269.56641°
Mean motion
3.76662 °/min
Orbital period
95.58 mins
BSTAR
0.00028895
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Other satellites on launch #207 in the year 2025 (2025-09-13 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-35251 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 | 2026-06-16 04:55:53.138Z | 191.841° SSW | 2026-06-16 04:58:53.138Z | 274.186° WNW | 35.824° | 2026-06-16 05:01:53.138Z | 333.358° NNW |
| 4 mins | 2026-06-16 16:33:53.138Z | 61.51° ENE | 2026-06-16 16:35:53.138Z | 102.507° ESE | 19.539° | 2026-06-16 16:37:53.138Z | 137.663° SSE |
| 4 mins | 2026-06-16 18:08:53.138Z | 321.541° NNW | 2026-06-16 18:09:53.138Z | 298.549° NW | 23.372° | 2026-06-16 18:12:53.138Z | 238.385° WSW |
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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