STARLINK-11567, 62909
Orbit data source: Space-Track
STARLINK-11567, 62909 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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62909 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 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-11567
1 62909U 25027C 26039.66569842 .00093930 00000-0 72692-3 0 9991
2 62909 42.9996 162.9499 0002189 297.6193 62.4453 15.70850227 58581Epoch: 2026-02-08T15:58Z
TLE epoch observation values (Epoch: 2026-02-08T15:58:36.343Z)
Latitude
0.00003°
Longitude
144.5269°
Altitude
355.555 km
Speed
7.698 km/s
True Right ascension
10h 51m 47s
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
04:51:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.922 km
Perigee altitude
356.973 km
Semi-major axis
6,736.584 km
Eccentricity
0.00022
Inclination
42.9996°
RAAN
162.9499°
Arg. of periapsis
297.6193°
True anomaly
62.46754°
Mean anomaly
62.4453°
Eccentric anomaly
62.45642°
Mean motion
3.9254 °/min
Orbital period
91.71 mins
BSTAR
0.00072692
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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-11567 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 | 2026-02-09 12:03:43.589Z | 235.975° WSW | 2026-02-09 12:05:43.589Z | 135.805° SSE | 41.722° | 2026-02-09 12:07:43.589Z | 77.933° E |
| 4 mins | 2026-02-09 15:16:43.589Z | 301.699° NW | 2026-02-09 15:17:43.589Z | 336.019° NNW | 38.519° | 2026-02-09 15:20:43.589Z | 92.186° ESE |
| 4 mins | 2026-02-09 16:52:43.589Z | 257.675° W | 2026-02-09 16:53:43.589Z | 225.647° WSW | 27.737° | 2026-02-09 16:56:43.589Z | 142.348° 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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