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, 14.5 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 25259.98377428 -.00003121 00000-0 -20943-4 0 9998
2 60727 53.1597 252.4876 0000125 113.5989 246.5042 15.69693252 61684Epoch: 2025-09-16T23:36Z
TLE epoch observation values (Epoch: 2025-09-16T23:36:38.097Z)
Latitude
-0.00004°
Longitude
-97.83741°
Altitude
360.723 km
Speed
7.694 km/s
True Right ascension
16h 49m 57s
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
04:20:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.12 km
Perigee altitude
359.951 km
Semi-major axis
6,738.172 km
Eccentricity
0.00001
Inclination
53.1597°
RAAN
252.4876°
Arg. of periapsis
113.5989°
True anomaly
246.50289°
Mean anomaly
246.5042°
Eccentric anomaly
246.50354°
Mean motion
3.92401 °/min
Orbital period
91.74 mins
BSTAR
-0.000020943
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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 | 2025-09-19 02:15:02.044Z | 258.086° W | 2025-09-19 02:17:02.044Z | 342.193° N | 34.465° | 2025-09-19 02:19:02.044Z | 35.194° NE |
| 4 mins | 2025-09-19 08:40:02.044Z | 302.846° NW | 2025-09-19 08:41:02.044Z | 285.84° WNW | 40.222° | 2025-09-19 08:44:02.044Z | 136.87° 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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