STARLINK-11627, 63107
Orbit data source: Space-Track
STARLINK-11627, 63107 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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63107 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-11627
1 63107U 25039D 26305.13797934 .00228667 00000-0 17361-2 0 9996
2 63107 42.9990 251.5237 0001181 271.5467 88.5265 15.70851365 96808Epoch: 2026-11-01T03:18Z
TLE epoch observation values (Epoch: 2026-11-01T03:18:41.414Z)
Latitude
-0.00006°
Longitude
161.41742°
Altitude
356.213 km
Speed
7.697 km/s
True Right ascension
16h 46m 05s
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
07:36:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.24 km
Perigee altitude
357.649 km
Semi-major axis
6,736.581 km
Eccentricity
0.00012
Inclination
42.999°
RAAN
251.5237°
Arg. of periapsis
271.5467°
True anomaly
88.54003°
Mean anomaly
88.5265°
Eccentric anomaly
88.53326°
Mean motion
3.9254 °/min
Orbital period
91.71 mins
BSTAR
0.0017361
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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-11627 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 | 2026-11-01 23:20:41.059Z | 189.775° SSW | 2026-11-01 23:22:41.059Z | 141.869° SSE | 19.082° | 2026-11-01 23:24:41.059Z | 98.956° ESE |
| 4 mins | 2026-11-02 00:56:41.059Z | 255.25° W | 2026-11-02 00:58:41.059Z | 56.759° ENE | 66.027° | 2026-11-02 01:00:41.059Z | 70.256° E |
| 4 mins | 2026-11-02 04:09:41.059Z | 295.414° NW | 2026-11-02 04:10:41.059Z | 332.145° NNW | 72.36° | 2026-11-02 04:13:41.059Z | 103.542° 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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