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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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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-11080
1 60727U 24152H 26163.85935354 .00001476 00000-0 17042-4 0 9992
2 60727 53.1587 7.0200 0001257 41.3061 318.8052 15.69708920103910Epoch: 2026-06-12T20:37Z
TLE epoch observation values (Epoch: 2026-06-12T20:37:28.145Z)
Latitude
-0.00003°
Longitude
156.46996°
Altitude
360.008 km
Speed
7.695 km/s
True Right ascension
00h 28m 04s
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
13:14:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.838 km
Perigee altitude
359.144 km
Semi-major axis
6,738.128 km
Eccentricity
0.00013
Inclination
53.1587°
RAAN
7.02°
Arg. of periapsis
41.3061°
True anomaly
318.79571°
Mean anomaly
318.8052°
Eccentric anomaly
318.80046°
Mean motion
3.92405 °/min
Orbital period
91.74 mins
BSTAR
0.000017042
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-13 16:42:03.068Z | 256.348° W | 2026-06-13 16:44:03.068Z | 339.055° N | 35.27° | 2026-06-13 16:46:03.068Z | 35.311° NE |
| 4 mins | 2026-06-13 23:07:03.068Z | 304.28° NW | 2026-06-13 23:09:03.068Z | 151.531° SSE | 39.766° | 2026-06-13 23:11:03.068Z | 135.942° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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