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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-11627
1 63107U 25039D 26104.46951810 .00142283 00000-0 10923-2 0 9990
2 63107 43.0024 21.0899 0000677 354.7506 5.3355 15.70866524 65243Epoch: 2026-04-14T11:16Z
TLE epoch observation values (Epoch: 2026-04-14T11:16:06.363Z)
Latitude
0°
Longitude
9.41807°
Altitude
355.737 km
Speed
7.698 km/s
True Right ascension
01h 24m 21s
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
05:33:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.857 km
Perigee altitude
357.944 km
Semi-major axis
6,736.537 km
Eccentricity
0.00007
Inclination
43.0024°
RAAN
21.0899°
Arg. of periapsis
354.7506°
True anomaly
5.33622°
Mean anomaly
5.3355°
Eccentric anomaly
5.33586°
Mean motion
3.92544 °/min
Orbital period
91.71 mins
BSTAR
0.0010923
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-14 23:46:03.796Z | 273.05° WNW | 2026-04-14 23:49:03.796Z | 2.767° NNE | 37.495° | 2026-04-14 23:51:03.796Z | 64.556° ENE |
| 4 mins | 2026-04-15 01:24:03.796Z | 307.427° NW | 2026-04-15 01:25:03.796Z | 351.815° N | 36.812° | 2026-04-15 01:28:03.796Z | 85.662° E |
| 4 mins | 2026-04-15 03:00:03.796Z | 266.167° W | 2026-04-15 03:01:03.796Z | 228.122° WSW | 35.314° | 2026-04-15 03:04:03.796Z | 130.255° SE |
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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