STARLINK-35415, 65885
Orbit data source: Space-Track
STARLINK-35415, 65885 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Oct 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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65885 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
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-35415
1 65885U 25224D 26062.13637353 .00028491 00000-0 97023-3 0 9992
2 65885 53.1619 41.6022 0001169 73.1254 286.9875 15.30205244 23773Epoch: 2026-03-03T03:16Z
TLE epoch observation values (Epoch: 2026-03-03T03:16:22.672Z)
Latitude
0.00001°
Longitude
-168.41203°
Altitude
475.865 km
Speed
7.629 km/s
True Right ascension
02h 46m 24s
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
17:49:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.257 km
Perigee altitude
474.654 km
Semi-major axis
6,853.593 km
Eccentricity
0.00012
Inclination
53.1619°
RAAN
41.6022°
Arg. of periapsis
73.1254°
True anomaly
286.97469°
Mean anomaly
286.9875°
Eccentric anomaly
286.98109°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00097023
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Other satellites on launch #224 in the year 2025 (2025-10-07 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-35415 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-04 01:25:28.514Z | 240.638° WSW | 2026-03-04 01:27:28.514Z | 340.578° N | 43.586° | 2026-03-04 01:30:28.514Z | 45.826° ENE |
| 4 mins | 2026-03-04 06:22:28.514Z | 350.208° N | 2026-03-04 06:24:28.514Z | 31.049° NE | 17.393° | 2026-03-04 06:26:28.514Z | 65.745° ENE |
| 5 mins | 2026-03-04 08:00:28.514Z | 309.416° NW | 2026-03-04 08:02:28.514Z | 156.377° SSE | 44.93° | 2026-03-04 08:05:28.514Z | 131.78° SE |
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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