STARLINK-34857, 65102
Orbit data source: Space-Track
STARLINK-34857, 65102 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 04 Aug 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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65102 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-34857
1 65102U 25167AA 26127.25071426 .00030774 00000-0 71358-3 0 9998
2 65102 53.1584 113.3730 0001117 74.3738 285.7392 15.42168764 42457Epoch: 2026-05-07T06:01Z
TLE epoch observation values (Epoch: 2026-05-07T06:01:01.712Z)
Latitude
0.00007°
Longitude
158.01637°
Altitude
440.408 km
Speed
7.649 km/s
True Right ascension
07h 33m 29s
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
00:47:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.729 km
Perigee altitude
439.206 km
Semi-major axis
6,818.105 km
Eccentricity
0.00011
Inclination
53.1584°
RAAN
113.373°
Arg. of periapsis
74.3738°
True anomaly
285.72688°
Mean anomaly
285.7392°
Eccentric anomaly
285.73304°
Mean motion
3.85521 °/min
Orbital period
93.38 mins
BSTAR
0.00071358
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Other satellites on launch #167 in the year 2025 (2025-08-04 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-34857 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 | 2026-05-08 00:50:10.976Z | 180.631° SSW | 2026-05-08 00:52:10.976Z | 142.64° SSE | 20.726° | 2026-05-08 00:55:10.976Z | 78.868° E |
| 4 mins | 2026-05-08 02:28:10.976Z | 277.175° WNW | 2026-05-08 02:29:10.976Z | 308.09° NW | 30.613° | 2026-05-08 02:32:10.976Z | 32.052° NE |
| 5 mins | 2026-05-08 08:59:10.976Z | 290.922° WNW | 2026-05-08 09:01:10.976Z | 233.867° WSW | 35.17° | 2026-05-08 09:04:10.976Z | 153.832° SSE |
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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