STARLINK-11080, 60727
Orbit data source: Space-Track
STARLINK-11080, 60727 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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60727 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-11080
1 60727U 24152H 25295.76592747 -.00004335 00000-0 -30965-4 0 9990
2 60727 53.1570 76.0933 0000870 83.1244 276.9873 15.69694994 67300Epoch: 2025-10-22T18:22Z
TLE epoch observation values (Epoch: 2025-10-22T18:22:56.133Z)
Latitude
-0°
Longitude
128.92458°
Altitude
360.613 km
Speed
7.694 km/s
True Right ascension
05h 04m 22s
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
13:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.617 km
Perigee altitude
359.445 km
Semi-major axis
6,738.168 km
Eccentricity
0.00009
Inclination
53.157°
RAAN
76.0933°
Arg. of periapsis
83.1244°
True anomaly
276.9774°
Mean anomaly
276.9873°
Eccentric anomaly
276.98235°
Mean motion
3.92401 °/min
Orbital period
91.74 mins
BSTAR
-0.000030965
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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-11080 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-23 19:20:31.048Z | 296.747° NW | 2025-10-23 19:22:31.048Z | 255.666° W | 33.19° | 2025-10-23 19:25:31.048Z | 151.392° SSE |
| 4 mins | 2025-10-24 11:50:31.048Z | 227.687° WSW | 2025-10-24 11:51:31.048Z | 224.276° SW | 41.803° | 2025-10-24 11:54:31.048Z | 50.542° ENE |
| 5 mins | 2025-10-24 18:14:31.048Z | 322.903° NNW | 2025-10-24 18:16:31.048Z | 25.505° NE | 37.965° | 2025-10-24 18:19:31.048Z | 115.361° 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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