STARLINK-11600, 63114
Orbit data source: Space-Track
STARLINK-11600, 63114 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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63114 intel report (Beta)
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Edit Public Description
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-11600
1 63114U 25039L 25312.85885345 .00214519 00000-0 16257-2 0 9998
2 63114 43.0010 245.0159 0001987 263.8014 96.2627 15.70939168 40612Epoch: 2025-11-08T20:36Z
TLE epoch observation values (Epoch: 2025-11-08T20:36:44.938Z)
Latitude
-0.00002°
Longitude
-112.4538°
Altitude
356.129 km
Speed
7.697 km/s
True Right ascension
16h 20m 03s
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
18:10:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.532 km
Perigee altitude
356.855 km
Semi-major axis
6,736.33 km
Eccentricity
0.0002
Inclination
43.001°
RAAN
245.0159°
Arg. of periapsis
263.8014°
True anomaly
96.28533°
Mean anomaly
96.2627°
Eccentric anomaly
96.27402°
Mean motion
3.92562 °/min
Orbital period
91.71 mins
BSTAR
0.0016257
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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-11600 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 | 2025-11-09 22:45:54.862Z | 209.364° SW | 2025-11-09 22:47:54.862Z | 150.704° SSE | 27.518° | 2025-11-09 22:49:54.862Z | 92.868° ESE |
| 4 mins | 2025-11-10 01:58:54.862Z | 306.64° NW | 2025-11-10 01:59:54.862Z | 346.796° N | 34.526° | 2025-11-10 02:02:54.862Z | 79.521° E |
| 4 mins | 2025-11-10 03:34:54.862Z | 278.773° WNW | 2025-11-10 03:35:54.862Z | 254.032° W | 39.778° | 2025-11-10 03:38:54.862Z | 119.271° 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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