STARLINK-5181, 54070
Orbit data source: Space-Track
STARLINK-5181, 54070 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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54070 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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-5181
1 54070U 22136V 25303.76219441 .00002344 00000-0 16528-3 0 9995
2 54070 53.2174 207.0844 0000815 92.0872 268.0214 15.08847497167232Epoch: 2025-10-30T18:17Z
TLE epoch observation values (Epoch: 2025-10-30T18:17:33.597Z)
Latitude
0.00004°
Longitude
-106.62189°
Altitude
540.637 km
Speed
7.593 km/s
True Right ascension
13h 48m 20s
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
20:13:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.529 km
Perigee altitude
539.402 km
Semi-major axis
6,918.102 km
Eccentricity
0.00008
Inclination
53.2174°
RAAN
207.0844°
Arg. of periapsis
92.0872°
True anomaly
268.01207°
Mean anomaly
268.0214°
Eccentric anomaly
268.01673°
Mean motion
3.77192 °/min
Orbital period
95.44 mins
BSTAR
0.00016528
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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-5181 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 01:04:14.016Z | 343.511° N | 2025-10-31 01:06:14.016Z | 15.436° NNE | 14.379° | 2025-10-31 01:08:14.016Z | 46.181° ENE |
| 5 mins | 2025-10-31 02:44:14.016Z | 335.098° NNW | 2025-10-31 02:46:14.016Z | 30.092° NE | 33.7° | 2025-10-31 02:49:14.016Z | 99.713° ESE |
| 5 mins | 2025-10-31 04:23:14.016Z | 277.233° WNW | 2025-10-31 04:25:14.016Z | 237.08° WSW | 24.759° | 2025-10-31 04:28:14.016Z | 176.965° S |
| 6 mins | 2025-10-31 19:54:14.016Z | 206.016° SW | 2025-10-31 19:57:14.016Z | 110.229° ESE | 37.75° | 2025-10-31 20:00:14.016Z | 60.063° ENE |
| 5 mins | 2025-10-31 21:34:14.016Z | 287.616° WNW | 2025-10-31 21:36:14.016Z | 329.736° NNW | 24.452° | 2025-10-31 21:39:14.016Z | 27.14° NE |
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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