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: 1 day ago
TLE from 1 day ago
0 STARLINK-11627
1 63107U 25039D 26150.31297330 .00221818 00000-0 16826-2 0 9995
2 63107 42.9997 104.7621 0001087 269.7332 90.3411 15.70895081 72458Epoch: 2026-05-30T07:30Z
TLE epoch observation values (Epoch: 2026-05-30T07:30:40.893Z)
Latitude
-0.00001°
Longitude
104.26091°
Altitude
356.113 km
Speed
7.697 km/s
True Right ascension
06h 59m 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
17:29:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.052 km
Perigee altitude
357.587 km
Semi-major axis
6,736.456 km
Eccentricity
0.00011
Inclination
42.9997°
RAAN
104.7621°
Arg. of periapsis
269.7332°
True anomaly
90.35356°
Mean anomaly
90.3411°
Eccentric anomaly
90.34733°
Mean motion
3.92551 °/min
Orbital period
91.71 mins
BSTAR
0.0016826
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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 | 2026-06-01 00:58:52.599Z | 256.607° W | 2026-06-01 00:59:52.599Z | 270.939° WNW | 42.989° | 2026-06-01 01:02:52.599Z | 70.879° E |
| 4 mins | 2026-06-01 02:34:52.599Z | 298.336° NW | 2026-06-01 02:36:52.599Z | 29.386° NE | 31.968° | 2026-06-01 02:38:52.599Z | 71.571° E |
| 4 mins | 2026-06-01 04:10:52.599Z | 291.233° WNW | 2026-06-01 04:12:52.599Z | 77.48° E | 43.345° | 2026-06-01 04:14:52.599Z | 103.921° 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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