STARLINK-5170, 54062
Orbit data source: Space-Track
STARLINK-5170, 54062 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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54062 intel report (Beta)
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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: 19 hours ago
TLE from 19 hours ago
0 STARLINK-5170
1 54062U 22136M 26312.25003472 .00022860 00000-0 68631-3 0 9993
2 54062 53.1592 309.5618 0001376 86.7894 197.1890 15.34368621 5824Epoch: 2026-11-08T06:00Z
TLE epoch observation values (Epoch: 2026-11-08T06:00:02.999Z)
Latitude
-51.11729°
Longitude
104.5961°
Altitude
481.386 km
Speed
7.624 km/s
True Right ascension
16h 08m 12s
True Declination
-50° 56' 32"
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
21:27:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.995 km
Perigee altitude
462.112 km
Semi-major axis
6,841.191 km
Eccentricity
0.00014
Inclination
53.1592°
RAAN
309.5618°
Arg. of periapsis
86.7894°
True anomaly
197.18434°
Mean anomaly
197.189°
Eccentric anomaly
197.18667°
Mean motion
3.83571 °/min
Orbital period
93.85 mins
BSTAR
0.00068631
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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-5170 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 | 2026-11-09 02:51:41.564Z | 241.182° WSW | 2026-11-09 02:53:41.564Z | 1.62° NNE | 68.276° | 2026-11-09 02:56:41.564Z | 46.132° ENE |
| 4 mins | 2026-11-09 07:47:41.564Z | 350.059° N | 2026-11-09 07:49:41.564Z | 30.232° NE | 17.52° | 2026-11-09 07:51:41.564Z | 64.732° ENE |
| 5 mins | 2026-11-09 09:25:41.564Z | 311.656° NW | 2026-11-09 09:27:41.564Z | 121.896° SE | 73.628° | 2026-11-09 09:30:41.564Z | 130.11° SE |
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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