STARLINK-11625, 63109
Orbit data source: Space-Track
STARLINK-11625, 63109 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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63109 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-11625
1 63109U 25039F 26104.49073821 .00129058 00000-0 98992-3 0 9990
2 63109 43.0030 21.2602 0004783 257.7489 102.2844 15.70921043 65248Epoch: 2026-04-14T11:46Z
TLE epoch observation values (Epoch: 2026-04-14T11:46:39.781Z)
Latitude
0.00004°
Longitude
1.92826°
Altitude
356.722 km
Speed
7.697 km/s
True Right ascension
01h 25m 02s
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
03:38:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
361.467 km
Perigee altitude
355.023 km
Semi-major axis
6,736.382 km
Eccentricity
0.00048
Inclination
43.003°
RAAN
21.2602°
Arg. of periapsis
257.7489°
True anomaly
102.33795°
Mean anomaly
102.2844°
Eccentric anomaly
102.31117°
Mean motion
3.92557 °/min
Orbital period
91.71 mins
BSTAR
0.00098992
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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-11625 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 | 2026-04-14 22:43:15.428Z | 242.482° WSW | 2026-04-14 22:45:15.428Z | 90.973° ESE | 40.305° | 2026-04-14 22:47:15.428Z | 74.118° E |
| 4 mins | 2026-04-15 00:19:15.428Z | 291.112° WNW | 2026-04-15 00:21:15.428Z | 13.419° NNE | 34.205° | 2026-04-15 00:23:15.428Z | 67.134° ENE |
| 4 mins | 2026-04-15 01:56:15.428Z | 302.949° NW | 2026-04-15 01:57:15.428Z | 3.659° NNE | 42.181° | 2026-04-15 02:00:15.428Z | 97.399° 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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