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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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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-5170
1 54062U 22136M 25303.92048488 .00001302 00000-0 99869-4 0 9998
2 54062 53.2172 206.6480 0001426 85.7541 274.3614 15.08837933167253Epoch: 2025-10-30T22:05Z
TLE epoch observation values (Epoch: 2025-10-30T22:05:29.893Z)
Latitude
-0.00004°
Longitude
-164.19893°
Altitude
540.572 km
Speed
7.593 km/s
True Right ascension
13h 46m 35s
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
02:50:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.981 km
Perigee altitude
539.008 km
Semi-major axis
6,918.132 km
Eccentricity
0.00014
Inclination
53.2172°
RAAN
206.648°
Arg. of periapsis
85.7541°
True anomaly
274.34511°
Mean anomaly
274.3614°
Eccentric anomaly
274.35325°
Mean motion
3.7719 °/min
Orbital period
95.44 mins
BSTAR
0.000099869
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-31 18:54:25.211Z | 158.942° S | 2025-10-31 18:56:25.211Z | 128.184° SE | 14.53° | 2025-10-31 18:58:25.211Z | 96.206° ESE |
| 7 mins | 2025-10-31 20:32:25.211Z | 238.416° WSW | 2025-10-31 20:35:25.211Z | 318.324° NNW | 43.538° | 2025-10-31 20:39:25.211Z | 46.499° ENE |
| 5 mins | 2025-11-01 01:34:25.211Z | 342.16° N | 2025-11-01 01:36:25.211Z | 19.37° NNE | 20.766° | 2025-11-01 01:39:25.211Z | 72.588° E |
| 6 mins | 2025-11-01 03:13:25.211Z | 306.165° NW | 2025-11-01 03:16:25.211Z | 202.016° SSW | 44.204° | 2025-11-01 03:19:25.211Z | 137.497° 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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