STARLINK-34890, 65760
Orbit data source: Space-Track
STARLINK-34890, 65760 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 25 Sep 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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65760 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-34890
1 65760U 25216AC 26171.38941576 .00021015 00000-0 71944-3 0 9997
2 65760 53.1589 215.4153 0000961 54.3466 305.7624 15.30209160 42260Epoch: 2026-06-20T09:20Z
TLE epoch observation values (Epoch: 2026-06-20T09:20:45.521Z)
Latitude
-0.00004°
Longitude
166.62086°
Altitude
475.702 km
Speed
7.629 km/s
True Right ascension
14h 21m 39s
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
07:12:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.103 km
Perigee altitude
474.786 km
Semi-major axis
6,853.581 km
Eccentricity
0.0001
Inclination
53.1589°
RAAN
215.4153°
Arg. of periapsis
54.3466°
True anomaly
305.75346°
Mean anomaly
305.7624°
Eccentric anomaly
305.75793°
Mean motion
3.82531 °/min
Orbital period
94.11 mins
BSTAR
0.00071944
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Other satellites on launch #216 in the year 2025 (2025-09-25 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-34890 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:55:56.122Z | 245.119° WSW | 2026-06-21 05:57:56.122Z | 329.714° NNW | 42.468° | 2026-06-21 06:00:56.122Z | 43.941° NE |
| 4 mins | 2026-06-21 10:52:56.122Z | 348.712° N | 2026-06-21 10:54:56.122Z | 30.168° NE | 18.268° | 2026-06-21 10:56:56.122Z | 66.491° ENE |
| 5 mins | 2026-06-21 12:30:56.122Z | 305.889° NW | 2026-06-21 12:32:56.122Z | 215.547° SW | 44.59° | 2026-06-21 12:35:56.122Z | 135.328° SSE |
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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