STARLINK-34906, 65896
Orbit data source: Space-Track
STARLINK-34906, 65896 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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65896 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-34906
1 65896U 25224Q 25340.61645575 .00052119 00000-0 17581-2 0 9994
2 65896 53.1622 83.7073 0001374 77.9174 282.1981 15.30227054 10622Epoch: 2025-12-06T14:47Z
TLE epoch observation values (Epoch: 2025-12-06T14:47:41.776Z)
Latitude
-0.00001°
Longitude
146.14159°
Altitude
475.835 km
Speed
7.629 km/s
True Right ascension
05h 34m 49s
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
03:08:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.332 km
Perigee altitude
474.449 km
Semi-major axis
6,853.527 km
Eccentricity
0.00014
Inclination
53.1622°
RAAN
83.7073°
Arg. of periapsis
77.9174°
True anomaly
282.18271°
Mean anomaly
282.1981°
Eccentric anomaly
282.19041°
Mean motion
3.82536 °/min
Orbital period
94.11 mins
BSTAR
0.0017581
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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-34906 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-07 09:46:36.802Z | 229.271° WSW | 2025-12-07 09:50:36.802Z | 47.378° ENE | 42.789° | 2025-12-07 09:53:36.802Z | 49.865° ENE |
| 4 mins | 2025-12-07 14:44:36.802Z | 341.638° N | 2025-12-07 14:46:36.802Z | 16.648° NNE | 16.111° | 2025-12-07 14:48:36.802Z | 54.162° ENE |
| 6 mins | 2025-12-07 16:22:36.802Z | 314.699° NW | 2025-12-07 16:25:36.802Z | 94.601° ESE | 42.258° | 2025-12-07 16:28:36.802Z | 125.011° SE |
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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