STARLINK-34680, 65356
Orbit data source: Space-Track
STARLINK-34680, 65356 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 28 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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65356 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-34680
1 65356U 25190F 26094.24708890 .00040780 00000-0 13813-2 0 9998
2 65356 53.1601 49.7853 0001195 85.3493 274.7644 15.30203508 33194Epoch: 2026-04-04T05:55Z
TLE epoch observation values (Epoch: 2026-04-04T05:55:48.480Z)
Latitude
-0.00007°
Longitude
128.26365°
Altitude
476.036 km
Speed
7.629 km/s
True Right ascension
03h 19m 08s
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
19:26:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.28 km
Perigee altitude
474.642 km
Semi-major axis
6,853.598 km
Eccentricity
0.00012
Inclination
53.1601°
RAAN
49.7853°
Arg. of periapsis
85.3493°
True anomaly
274.75075°
Mean anomaly
274.7644°
Eccentric anomaly
274.75758°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.0013813
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Other satellites on launch #190 in the year 2025 (2025-08-28 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-34680 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 | 2026-04-04 23:19:57.221Z | 211.532° SW | 2026-04-04 23:22:57.221Z | 160.786° S | 36.997° | 2026-04-04 23:25:57.221Z | 63.321° ENE |
| 4 mins | 2026-04-05 00:59:57.221Z | 297.43° NW | 2026-04-05 01:00:57.221Z | 319.985° NNW | 21.711° | 2026-04-05 01:03:57.221Z | 23.863° NE |
| 5 mins | 2026-04-05 05:55:57.221Z | 327.817° NNW | 2026-04-05 05:57:57.221Z | 15.788° NNE | 34.644° | 2026-04-05 06:00:57.221Z | 104.092° ESE |
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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