STARLINK-11560, 62917
Orbit data source: Space-Track
STARLINK-11560, 62917 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Feb 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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62917 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 STARLINK-11560
1 62917U 25027L 26305.85413889 .00213291 00000-0 15693-2 0 9997
2 62917 42.9992 357.9616 0001224 41.1783 318.9177 15.71646492100453Epoch: 2026-11-01T20:29Z
TLE epoch observation values (Epoch: 2026-11-01T20:29:57.600Z)
Latitude
-0.00001°
Longitude
9.33205°
Altitude
353.341 km
Speed
7.699 km/s
True Right ascension
23h 51m 50s
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
07:41:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
356.998 km
Perigee altitude
355.349 km
Semi-major axis
6,734.31 km
Eccentricity
0.00012
Inclination
42.9992°
RAAN
357.9616°
Arg. of periapsis
41.1783°
True anomaly
318.90848°
Mean anomaly
318.9177°
Eccentric anomaly
318.91309°
Mean motion
3.92739 °/min
Orbital period
91.66 mins
BSTAR
0.0015693
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Other satellites on launch #27 in the year 2025 (2025-02-08 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-11560 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-02 12:12:40.541Z | 276.177° WNW | 2026-11-02 12:14:40.541Z | 209.125° SW | 48.631° | 2026-11-02 12:16:40.541Z | 134.812° SE |
| 4 mins | 2026-11-03 09:27:40.541Z | 306.701° NW | 2026-11-03 09:28:40.541Z | 348.9° N | 41.55° | 2026-11-03 09:31:40.541Z | 74.425° E |
| 4 mins | 2026-11-03 11:03:40.541Z | 290.997° WNW | 2026-11-03 11:04:40.541Z | 299.75° NW | 64.9° | 2026-11-03 11:07:40.541Z | 106.793° 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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