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, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-5160
1 54080U 22136AF 25260.61653306 .00000783 00000-0 67258-4 0 9996
2 54080 53.2167 36.2404 0000993 69.0737 291.0361 15.08836383160784Epoch: 2025-09-17T14:47Z
TLE epoch observation values (Epoch: 2025-09-17T14:47:48.456Z)
Latitude
-0.00005°
Longitude
177.49854°
Altitude
540.405 km
Speed
7.593 km/s
True Right ascension
02h 24m 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
05:02:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.686 km
Perigee altitude
539.313 km
Semi-major axis
6,918.136 km
Eccentricity
0.0001
Inclination
53.2167°
RAAN
36.2404°
Arg. of periapsis
69.0737°
True anomaly
291.02548°
Mean anomaly
291.0361°
Eccentric anomaly
291.03079°
Mean motion
3.77189 °/min
Orbital period
95.44 mins
BSTAR
0.000067258
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 13:18:25.179Z | 287.181° WNW | 2025-09-18 13:21:25.179Z | 343.284° N | 21.391° | 2025-09-18 13:23:25.179Z | 19.838° NNE |
| 6 mins | 2025-09-18 18:19:25.179Z | 317.681° NNW | 2025-09-18 18:22:25.179Z | 51.748° ENE | 42.421° | 2025-09-18 18:25:25.179Z | 118.942° SE |
| 6 mins | 2025-09-19 11:30:25.179Z | 229.81° WSW | 2025-09-19 11:32:25.179Z | 235.094° WSW | 44.273° | 2025-09-19 11:36:25.179Z | 49.711° ENE |
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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