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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-11584
1 63106U 25039C 26305.00002315 -.00026961 00000-0 -20737-3 0 9990
2 63106 43.0000 252.8056 0001678 248.0327 230.5779 15.70830113 5952Epoch: 2026-11-01T00:00Z
TLE epoch observation values (Epoch: 2026-11-01T00:00:02.000Z)
Latitude
36.92682°
Longitude
-20.7661°
Altitude
359.049 km
Speed
7.699 km/s
True Right ascension
01h 18m 09s
True Declination
36° 45' 07"
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
07:36:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.635 km
Perigee altitude
357.374 km
Semi-major axis
6,736.642 km
Eccentricity
0.00017
Inclination
43°
RAAN
252.8056°
Arg. of periapsis
248.0327°
True anomaly
230.56305°
Mean anomaly
230.5779°
Eccentric anomaly
230.57047°
Mean motion
3.92535 °/min
Orbital period
91.71 mins
BSTAR
-0.00020737
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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 | 2026-11-02 00:08:14.073Z | 224.344° SW | 2026-11-02 00:10:14.073Z | 176.502° S | 41.423° | 2026-11-02 00:13:14.073Z | 81.439° E |
| 4 mins | 2026-11-02 01:45:14.073Z | 284.209° WNW | 2026-11-02 01:46:14.073Z | 315.761° NNW | 45.552° | 2026-11-02 01:49:14.073Z | 66.768° ENE |
| 4 mins | 2026-11-02 03:21:14.073Z | 299.167° NW | 2026-11-02 03:23:14.073Z | 23.184° NE | 47.308° | 2026-11-02 03:25:14.073Z | 80.411° 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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