STARLINK-11266, 60732
Orbit data source: Space-Track
STARLINK-11266, 60732 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 28 Aug 2024 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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60732 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: 3 hours ago
TLE from 3 hours ago
0 STARLINK-11266
1 60732U 24152N 25300.51659786 .00000588 00000-0 97140-5 0 9996
2 60732 53.1574 52.3769 0000968 63.2247 296.8869 15.69708617 67926Epoch: 2025-10-27T12:23Z
TLE epoch observation values (Epoch: 2025-10-27T12:23:54.055Z)
Latitude
-0.00007°
Longitude
-169.7157°
Altitude
360.351 km
Speed
7.694 km/s
True Right ascension
03h 29m 30s
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
11:00:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.644 km
Perigee altitude
359.34 km
Semi-major axis
6,738.129 km
Eccentricity
0.0001
Inclination
53.1574°
RAAN
52.3769°
Arg. of periapsis
63.2247°
True anomaly
296.87701°
Mean anomaly
296.8869°
Eccentric anomaly
296.88195°
Mean motion
3.92405 °/min
Orbital period
91.74 mins
BSTAR
0.000009714
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Other satellites on launch #152 in the year 2024 (2024-08-28 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-11266 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 | 2025-10-27 17:30:19.205Z | 301.712° NW | 2025-10-27 17:31:19.205Z | 249.373° W | 44.063° | 2025-10-27 17:34:19.205Z | 135.487° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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