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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-35415
1 65885U 25224D 25312.73766397 .00142742 00000-0 25213-2 0 9993
2 65885 53.1595 214.0380 0000980 63.0067 297.1042 15.49384012 6243Epoch: 2025-11-08T17:42Z
TLE epoch observation values (Epoch: 2025-11-08T17:42:14.167Z)
Latitude
-0.00006°
Longitude
-99.68404°
Altitude
419.131 km
Speed
7.661 km/s
True Right ascension
14h 16m 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
04:04:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.452 km
Perigee altitude
418.119 km
Semi-major axis
6,796.922 km
Eccentricity
0.0001
Inclination
53.1595°
RAAN
214.038°
Arg. of periapsis
63.0067°
True anomaly
297.0942°
Mean anomaly
297.1042°
Eccentric anomaly
297.0992°
Mean motion
3.87324 °/min
Orbital period
92.95 mins
BSTAR
0.0025213
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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 | 2025-11-10 19:24:36.139Z | 206.103° SW | 2025-11-10 19:26:36.139Z | 155.613° SSE | 36.152° | 2025-11-10 19:29:36.139Z | 62.359° ENE |
| 5 mins | 2025-11-11 01:54:36.139Z | 333.128° NNW | 2025-11-11 01:56:36.139Z | 33.255° NE | 31.625° | 2025-11-11 01:59:36.139Z | 103.535° ESE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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