STARLINK-11565, 62912
Orbit data source: Space-Track
STARLINK-11565, 62912 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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62912 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: 2 days ago
TLE from 2 days ago
0 STARLINK-11565
1 62912U 25027F 26185.85387907 .00161148 00000-0 12326-2 0 9992
2 62912 42.9990 1.0226 0001606 273.6552 86.4132 15.70889719 81580Epoch: 2026-07-04T20:29Z
TLE epoch observation values (Epoch: 2026-07-04T20:29:35.151Z)
Latitude
-0.00002°
Longitude
130.76451°
Altitude
356.057 km
Speed
7.697 km/s
True Right ascension
00h 04m 05s
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
22:25:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.417 km
Perigee altitude
357.253 km
Semi-major axis
6,736.472 km
Eccentricity
0.00016
Inclination
42.999°
RAAN
1.0226°
Arg. of periapsis
273.6552°
True anomaly
86.43157°
Mean anomaly
86.4132°
Eccentric anomaly
86.42238°
Mean motion
3.9255 °/min
Orbital period
91.71 mins
BSTAR
0.0012326
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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-11565 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 | 2026-07-06 15:28:46.935Z | 245.633° WSW | 2026-07-06 15:29:46.935Z | 234.458° WSW | 41.89° | 2026-07-06 15:32:46.935Z | 73.016° E |
| 4 mins | 2026-07-06 17:04:46.935Z | 294.579° NW | 2026-07-06 17:06:46.935Z | 24.283° NE | 32.754° | 2026-07-06 17:08:46.935Z | 69.098° E |
| 4 mins | 2026-07-06 18:40:46.935Z | 294.034° NW | 2026-07-06 18:42:46.935Z | 39.16° NE | 42.564° | 2026-07-06 18:44:46.935Z | 96.876° 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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