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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-11607
1 63140U 25043J 26255.86936071 .00170180 00000-0 13007-2 0 9998
2 63140 43.0009 202.1873 0002000 262.1759 97.8881 15.70878218 88913Epoch: 2026-09-12T20:51Z
TLE epoch observation values (Epoch: 2026-09-12T20:51:52.765Z)
Latitude
-0.00006°
Longitude
-102.65479°
Altitude
356.342 km
Speed
7.697 km/s
True Right ascension
13h 28m 44s
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
00:43:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.715 km
Perigee altitude
357.02 km
Semi-major axis
6,736.504 km
Eccentricity
0.0002
Inclination
43.0009°
RAAN
202.1873°
Arg. of periapsis
262.1759°
True anomaly
97.9108°
Mean anomaly
97.8881°
Eccentric anomaly
97.89945°
Mean motion
3.92547 °/min
Orbital period
91.71 mins
BSTAR
0.0013007
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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 | 2026-09-14 00:35:40.073Z | 247.329° WSW | 2026-09-14 00:37:40.073Z | 79.283° E | 59.05° | 2026-09-14 00:39:40.073Z | 72.474° E |
| 4 mins | 2026-09-14 02:11:40.073Z | 293.068° NW | 2026-09-14 02:13:40.073Z | 14.028° NNE | 41.759° | 2026-09-14 02:15:40.073Z | 67.303° ENE |
| 4 mins | 2026-09-14 03:48:40.073Z | 302.286° NW | 2026-09-14 03:49:40.073Z | 7.577° NNE | 67.718° | 2026-09-14 03:52:40.073Z | 99.1° 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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