STARLINK-11265, 60909
Orbit data source: Space-Track
STARLINK-11265, 60909 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 31 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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60909 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-11265
1 60909U 24154G 26129.45717963 -.00002448 00000-0 -15367-4 0 9998
2 60909 53.1593 192.0669 0001042 73.2027 286.9105 15.69691690 98058Epoch: 2026-05-09T10:58Z
TLE epoch observation values (Epoch: 2026-05-09T10:58:20.320Z)
Latitude
-0.00001°
Longitude
160.20789°
Altitude
360.49 km
Speed
7.694 km/s
True Right ascension
12h 48m 16s
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
19:50:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.742 km
Perigee altitude
359.338 km
Semi-major axis
6,738.177 km
Eccentricity
0.0001
Inclination
53.1593°
RAAN
192.0669°
Arg. of periapsis
73.2027°
True anomaly
286.89908°
Mean anomaly
286.9105°
Eccentric anomaly
286.90479°
Mean motion
3.92401 °/min
Orbital period
91.74 mins
BSTAR
-0.000015367
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Other satellites on launch #154 in the year 2024 (2024-08-31 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-11265 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 | 2026-05-10 13:27:16.207Z | 319.411° NNW | 2026-05-10 13:29:16.207Z | 91.822° ESE | 40.151° | 2026-05-10 13:31:16.207Z | 122.013° SE |
| 4 mins | 2026-05-11 05:56:16.207Z | 187.636° SSW | 2026-05-11 05:58:16.207Z | 112.974° SE | 27.675° | 2026-05-11 06:00:16.207Z | 69.293° E |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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