STARLINK-34796, 65205
Orbit data source: Space-Track
STARLINK-34796, 65205 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 14 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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65205 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: 1 day ago
TLE from 1 day ago
0 STARLINK-34796
1 65205U 25176H 26095.25724545 .00005912 00000-0 21171-3 0 9997
2 65205 53.1607 29.6388 0000726 106.4791 253.6289 15.30176280 37188Epoch: 2026-04-05T06:10Z
TLE epoch observation values (Epoch: 2026-04-05T06:10:26.006Z)
Latitude
-0.00009°
Longitude
103.46511°
Altitude
476.326 km
Speed
7.629 km/s
True Right ascension
01h 58m 33s
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
12:23:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.04 km
Perigee altitude
475.045 km
Semi-major axis
6,853.679 km
Eccentricity
0.00007
Inclination
53.1607°
RAAN
29.6388°
Arg. of periapsis
106.4791°
True anomaly
253.62092°
Mean anomaly
253.6289°
Eccentric anomaly
253.62491°
Mean motion
3.82523 °/min
Orbital period
94.11 mins
BSTAR
0.00021171
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Other satellites on launch #176 in the year 2025 (2025-08-14 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-34796 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-06 21:31:58.646Z | 204.988° SW | 2026-04-06 21:34:58.646Z | 114.731° SE | 35.636° | 2026-04-06 21:37:58.646Z | 61.085° ENE |
| 4 mins | 2026-04-06 23:10:58.646Z | 291.609° WNW | 2026-04-06 23:12:58.646Z | 340.557° N | 22.921° | 2026-04-06 23:14:58.646Z | 21.535° NNE |
| 5 mins | 2026-04-07 04:07:58.646Z | 338.809° N | 2026-04-07 04:09:58.646Z | 53.134° ENE | 33.19° | 2026-04-07 04:12:58.646Z | 106.474° ESE |
| 4 mins | 2026-04-07 05:45:58.646Z | 261.204° W | 2026-04-07 05:46:58.646Z | 238.654° WSW | 20.727° | 2026-04-07 05:49:58.646Z | 179.817° S |
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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