STARLINK-11607, 63140
Orbit data source: Space-Track
STARLINK-11607, 63140 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 03 Mar 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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63140 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-11607
1 63140U 25043J 26306.41668981 -.00056629 00000-0 -44035-3 0 9997
2 63140 43.0001 257.5056 0001796 266.0703 86.6614 15.70864453 5965Epoch: 2026-11-02T10:00Z
TLE epoch observation values (Epoch: 2026-11-02T10:00:01.999Z)
Latitude
-5.02466°
Longitude
60.42357°
Altitude
356.915 km
Speed
7.697 km/s
True Right ascension
16h 48m 30s
True Declination
-4° 59' 35"
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
06:07:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.617 km
Perigee altitude
357.197 km
Semi-major axis
6,736.544 km
Eccentricity
0.00018
Inclination
43.0001°
RAAN
257.5056°
Arg. of periapsis
266.0703°
True anomaly
86.68195°
Mean anomaly
86.6614°
Eccentric anomaly
86.67167°
Mean motion
3.92543 °/min
Orbital period
91.71 mins
BSTAR
-0.00044035
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Other satellites on launch #43 in the year 2025 (2025-03-03 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-11607 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 | 2026-11-04 02:02:37.769Z | 297.745° NW | 2026-11-04 02:03:37.769Z | 342.208° N | 45.048° | 2026-11-04 02:06:37.769Z | 69.294° E |
| 4 mins | 2026-11-04 03:38:37.769Z | 300.912° NW | 2026-11-04 03:40:37.769Z | 52.855° ENE | 48.081° | 2026-11-04 03:42:37.769Z | 89.734° E |
| 4 mins | 2026-11-04 05:14:37.769Z | 263.402° W | 2026-11-04 05:16:37.769Z | 186.534° SSW | 33.679° | 2026-11-04 05:18:37.769Z | 141.993° SSE |
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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