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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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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-11584
1 63106U 25039C 25257.26075914 .00128004 00000-0 98504-3 0 9994
2 63106 42.9989 220.6716 0001648 270.6062 89.4617 15.70857391 31864Epoch: 2025-09-14T06:15Z
TLE epoch observation values (Epoch: 2025-09-14T06:15:29.589Z)
Latitude
-0.00001°
Longitude
133.31599°
Altitude
356.206 km
Speed
7.697 km/s
True Right ascension
14h 42m 41s
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
23:27:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.537 km
Perigee altitude
357.317 km
Semi-major axis
6,736.564 km
Eccentricity
0.00016
Inclination
42.9989°
RAAN
220.6716°
Arg. of periapsis
270.6062°
True anomaly
89.48058°
Mean anomaly
89.4617°
Eccentric anomaly
89.47114°
Mean motion
3.92541 °/min
Orbital period
91.71 mins
BSTAR
0.00098504
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-16 02:50:42.922Z | 298.744° NW | 2025-09-16 02:51:42.922Z | 341.419° N | 34.685° | 2025-09-16 02:54:42.922Z | 70.333° E |
| 4 mins | 2025-09-16 04:26:42.922Z | 298.937° NW | 2025-09-16 04:28:42.922Z | 61.872° ENE | 37.442° | 2025-09-16 04:30:42.922Z | 93.555° ESE |
| 4 mins | 2025-09-16 06:02:42.922Z | 257.779° W | 2025-09-16 06:03:42.922Z | 228.907° WSW | 25.563° | 2025-09-16 06:06:42.922Z | 145.933° 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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