STARLINK-5160, 54080
Orbit data source: Space-Track
STARLINK-5160, 54080 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 20 Oct 2022 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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54080 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, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-5160
1 54080U 22136AF 25317.51674997 -.00001489 00000-0 -75515-4 0 9998
2 54080 53.2146 140.8048 0001275 94.7170 265.3967 15.08828095169378Epoch: 2025-11-13T12:24Z
TLE epoch observation values (Epoch: 2025-11-13T12:24:07.197Z)
Latitude
-0.00008°
Longitude
-98.09872°
Altitude
540.748 km
Speed
7.593 km/s
True Right ascension
09h 23m 13s
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
19:53:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.907 km
Perigee altitude
539.143 km
Semi-major axis
6,918.162 km
Eccentricity
0.00013
Inclination
53.2146°
RAAN
140.8048°
Arg. of periapsis
94.717°
True anomaly
265.38214°
Mean anomaly
265.3967°
Eccentric anomaly
265.38942°
Mean motion
3.77187 °/min
Orbital period
95.44 mins
BSTAR
-0.000075515
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Other satellites on launch #136 in the year 2022 (2022-10-20 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-5160 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-14 13:59:24.757Z | 181.316° SSW | 2025-11-14 14:02:24.757Z | 124.076° SE | 23.481° | 2025-11-14 14:05:24.757Z | 74.209° E |
| 5 mins | 2025-11-14 15:39:24.757Z | 267.851° W | 2025-11-14 15:41:24.757Z | 328.861° NNW | 34.884° | 2025-11-14 15:44:24.757Z | 35.265° NE |
| 5 mins | 2025-11-14 20:40:24.757Z | 338.513° N | 2025-11-14 20:42:24.757Z | 21.125° NNE | 26.702° | 2025-11-14 20:45:24.757Z | 84.896° E |
| 6 mins | 2025-11-14 22:19:24.757Z | 291.508° WNW | 2025-11-14 22:22:24.757Z | 212.39° SW | 34.145° | 2025-11-14 22:25:24.757Z | 156.999° SSE |
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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