STARLINK-35027, 65466
Orbit data source: Space-Track
STARLINK-35027, 65466 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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65466 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-35027
1 65466U 25195J 26101.28813623 .00009314 00000-0 32626-3 0 9991
2 65466 53.1589 106.8355 0001270 88.5764 271.5382 15.30193692 34987Epoch: 2026-04-11T06:54Z
TLE epoch observation values (Epoch: 2026-04-11T06:54:54.970Z)
Latitude
-0.00003°
Longitude
163.59684°
Altitude
476.11 km
Speed
7.629 km/s
True Right ascension
07h 07m 20s
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
21:45:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.361 km
Perigee altitude
474.62 km
Semi-major axis
6,853.628 km
Eccentricity
0.00013
Inclination
53.1589°
RAAN
106.8355°
Arg. of periapsis
88.5764°
True anomaly
271.52365°
Mean anomaly
271.5382°
Eccentric anomaly
271.53093°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.00032626
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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-35027 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-12 01:52:52.514Z | 166.913° S | 2026-04-12 01:54:52.514Z | 129.743° SE | 17.445° | 2026-04-12 01:56:52.514Z | 91.526° ESE |
| 5 mins | 2026-04-12 03:30:52.514Z | 260.51° W | 2026-04-12 03:32:52.514Z | 344.735° N | 37.175° | 2026-04-12 03:35:52.514Z | 40.621° NE |
| 4 mins | 2026-04-12 08:27:52.514Z | 350.988° N | 2026-04-12 08:29:52.514Z | 37.561° NE | 20.405° | 2026-04-12 08:31:52.514Z | 74.201° E |
| 5 mins | 2026-04-12 10:05:52.514Z | 293.549° NW | 2026-04-12 10:07:52.514Z | 196.803° SSW | 40.071° | 2026-04-12 10:10:52.514Z | 144.258° SSE |
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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