STARLINK-11624, 63105
Orbit data source: Space-Track
STARLINK-11624, 63105 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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63105 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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-11624
1 63105U 25039B 26067.81478895 .00316467 00000-0 23693-2 0 9997
2 63105 43.0004 242.4970 0002040 269.7895 90.2739 15.70918221 59479Epoch: 2026-03-08T19:33Z
TLE epoch observation values (Epoch: 2026-03-08T19:33:17.765Z)
Latitude
-0°
Longitude
142.6563°
Altitude
356.05 km
Speed
7.697 km/s
True Right ascension
16h 09m 59s
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
16:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.627 km
Perigee altitude
356.879 km
Semi-major axis
6,736.39 km
Eccentricity
0.0002
Inclination
43.0004°
RAAN
242.497°
Arg. of periapsis
269.7895°
True anomaly
90.29728°
Mean anomaly
90.2739°
Eccentric anomaly
90.28559°
Mean motion
3.92557 °/min
Orbital period
91.71 mins
BSTAR
0.0023693
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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-11624 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 | 2026-03-09 15:39:05.057Z | 238.694° WSW | 2026-03-09 15:40:05.057Z | 213.892° SW | 41.564° | 2026-03-09 15:43:05.057Z | 74.494° E |
| 4 mins | 2026-03-09 17:15:05.057Z | 293.514° NW | 2026-03-09 17:17:05.057Z | 26.887° NE | 32.577° | 2026-03-09 17:19:05.057Z | 68.6° E |
| 4 mins | 2026-03-09 18:51:05.057Z | 295.781° NW | 2026-03-09 18:53:05.057Z | 38.633° NE | 41.057° | 2026-03-09 18:55:05.057Z | 93.363° 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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