STARLINK-11584, 63106
Orbit data source: Space-Track
STARLINK-11584, 63106 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 27 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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63106 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: 7 hours ago
TLE from 7 hours ago
0 STARLINK-11584
1 63106U 25039C 26150.98066448 .00103617 00000-0 80041-3 0 9998
2 63106 43.0004 101.1875 0001694 250.2963 109.7722 15.70856682 72554Epoch: 2026-05-30T23:32Z
TLE epoch observation values (Epoch: 2026-05-30T23:32:09.411Z)
Latitude
0°
Longitude
-140.34062°
Altitude
356.605 km
Speed
7.697 km/s
True Right ascension
06h 44m 45s
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
16:35:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.57 km
Perigee altitude
357.288 km
Semi-major axis
6,736.566 km
Eccentricity
0.00017
Inclination
43.0004°
RAAN
101.1875°
Arg. of periapsis
250.2963°
True anomaly
109.79047°
Mean anomaly
109.7722°
Eccentric anomaly
109.78133°
Mean motion
3.92541 °/min
Orbital period
91.71 mins
BSTAR
0.00080041
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Other satellites on launch #39 in the year 2025 (2025-02-27 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-11584 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 | 2026-06-01 00:10:26.901Z | 225.209° WSW | 2026-06-01 00:12:26.901Z | 177.915° S | 33.594° | 2026-06-01 00:15:26.901Z | 81.387° E |
| 4 mins | 2026-06-01 01:47:26.901Z | 284.435° WNW | 2026-06-01 01:48:26.901Z | 316.276° NNW | 35.492° | 2026-06-01 01:51:26.901Z | 67.333° ENE |
| 4 mins | 2026-06-01 03:23:26.901Z | 298.861° NW | 2026-06-01 03:25:26.901Z | 27.058° NE | 36.569° | 2026-06-01 03:27:26.901Z | 81.925° E |
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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