STARLINK-5167, 54058
Orbit data source: Space-Track
STARLINK-5167, 54058 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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54058 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-5167
1 54058U 22136H 25365.19623514 .00000812 00000-0 69098-4 0 9995
2 54058 53.2184 291.6077 0001321 92.9960 267.1183 15.08840846176502Epoch: 2025-12-31T04:42Z
TLE epoch observation values (Epoch: 2025-12-31T04:42:34.716Z)
Latitude
-0.00003°
Longitude
121.0944°
Altitude
540.684 km
Speed
7.593 km/s
True Right ascension
19h 26m 25s
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
15:19:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.899 km
Perigee altitude
539.072 km
Semi-major axis
6,918.123 km
Eccentricity
0.00013
Inclination
53.2184°
RAAN
291.6077°
Arg. of periapsis
92.996°
True anomaly
267.10318°
Mean anomaly
267.1183°
Eccentric anomaly
267.11074°
Mean motion
3.77191 °/min
Orbital period
95.44 mins
BSTAR
0.000069098
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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-5167 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 | 2025-12-31 20:45:58.160Z | 158.18° S | 2025-12-31 20:47:58.160Z | 122.591° SE | 17.074° | 2025-12-31 20:49:58.160Z | 89.813° E |
| 6 mins | 2025-12-31 22:23:58.160Z | 246.098° WSW | 2025-12-31 22:26:58.160Z | 343.815° N | 40.719° | 2025-12-31 22:29:58.160Z | 42.002° NE |
| 5 mins | 2026-01-01 03:25:58.160Z | 344.742° N | 2026-01-01 03:27:58.160Z | 26.036° NE | 22.505° | 2026-01-01 03:30:58.160Z | 78.57° E |
| 6 mins | 2026-01-01 05:04:58.160Z | 300.664° NW | 2026-01-01 05:07:58.160Z | 188.263° SSW | 40.88° | 2026-01-01 05:10:58.160Z | 143.329° 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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