STARLINK-35050, 65440
Orbit data source: Space-Track
STARLINK-35050, 65440 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Wed, 03 Sep 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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65440 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-35050
1 65440U 25194G 26171.31401981 .00009174 00000-0 63864-3 0 9995
2 65440 97.3381 24.5067 0002839 85.6004 274.5548 15.05665217 45092Epoch: 2026-06-20T07:32Z
TLE epoch observation values (Epoch: 2026-06-20T07:32:11.311Z)
Latitude
-0.00001°
Longitude
2.92915°
Altitude
552.382 km
Speed
7.586 km/s
True Right ascension
01h 38m 01s
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
07:21:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.412 km
Perigee altitude
544.481 km
Semi-major axis
6,924.584 km
Eccentricity
0.00028
Inclination
97.3381°
RAAN
24.5067°
Arg. of periapsis
85.6004°
True anomaly
274.52237°
Mean anomaly
274.5548°
Eccentric anomaly
274.53858°
Mean motion
3.76663 °/min
Orbital period
95.58 mins
BSTAR
0.00063864
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Other satellites on launch #194 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-35050 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 03:13:42.966Z | 6.91° NNE | 2026-06-21 03:17:42.966Z | 263.638° W | 43.034° | 2026-06-21 03:20:42.966Z | 201.872° SSW |
| 6 mins | 2026-06-21 13:58:42.966Z | 145.714° SSE | 2026-06-21 14:01:42.966Z | 53.247° ENE | 37.568° | 2026-06-21 14:04:42.966Z | 0.003° NNE |
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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