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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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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-34580
1 65808U 25218T 26062.59981771 .00007397 00000-0 51614-3 0 9994
2 65808 97.6021 286.9569 0001994 65.7589 294.3846 15.05662372 24056Epoch: 2026-03-03T14:23Z
TLE epoch observation values (Epoch: 2026-03-03T14:23:44.250Z)
Latitude
-0°
Longitude
-90.35403°
Altitude
551.968 km
Speed
7.586 km/s
True Right ascension
19h 07m 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
02:49:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.847 km
Perigee altitude
545.086 km
Semi-major axis
6,924.604 km
Eccentricity
0.0002
Inclination
97.6021°
RAAN
286.9569°
Arg. of periapsis
65.7589°
True anomaly
294.36379°
Mean anomaly
294.3846°
Eccentric anomaly
294.37419°
Mean motion
3.76661 °/min
Orbital period
95.58 mins
BSTAR
0.00051614
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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 | 2026-03-04 03:43:23.115Z | 13.738° NNE | 2026-03-04 03:46:23.115Z | 77.259° E | 44.886° | 2026-03-04 03:49:23.115Z | 191.05° SSW |
| 5 mins | 2026-03-04 14:28:23.115Z | 127.49° SE | 2026-03-04 14:30:23.115Z | 67.438° ENE | 32.942° | 2026-03-04 14:33:23.115Z | 6.098° NNE |
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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