STARLINK-34580, 65808
Orbit data source: Space-Track
STARLINK-34580, 65808 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Fri, 26 Sep 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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65808 intel report (Beta)
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Edit Public Description
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
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-34580
1 65808U 25218T 26014.08523017 .00004559 00000-0 31997-3 0 9999
2 65808 97.6040 239.1388 0002459 85.0726 275.0781 15.05652530 16758Epoch: 2026-01-14T02:02Z
TLE epoch observation values (Epoch: 2026-01-14T02:02:43.886Z)
Latitude
-0.00008°
Longitude
94.89767°
Altitude
552.418 km
Speed
7.586 km/s
True Right ascension
15h 56m 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
18:15:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.2 km
Perigee altitude
544.794 km
Semi-major axis
6,924.634 km
Eccentricity
0.00025
Inclination
97.604°
RAAN
239.1388°
Arg. of periapsis
85.0726°
True anomaly
275.05003°
Mean anomaly
275.0781°
Eccentric anomaly
275.06407°
Mean motion
3.76659 °/min
Orbital period
95.58 mins
BSTAR
0.00031997
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Other satellites on launch #218 in the year 2025 (2025-09-26 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-34580 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 | 2026-01-15 04:08:11.111Z | 352.612° N | 2026-01-15 04:11:11.111Z | 263.235° W | 34.66° | 2026-01-15 04:14:11.111Z | 214.159° SW |
| 6 mins | 2026-01-15 14:52:11.111Z | 163.233° S | 2026-01-15 14:54:11.111Z | 145.853° SSE | 43.661° | 2026-01-15 14:58:11.111Z | 349.482° N |
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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