STARLINK-30551, 58083
Orbit data source: Space-Track
STARLINK-30551, 58083 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 18 Oct 2023 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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58083 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-30551
1 58083U 23160J 26171.13298049 -.00000143 00000-0 43306-5 0 9999
2 58083 42.9991 222.7033 0000909 227.5187 132.5588 15.27581184148578Epoch: 2026-06-20T03:11Z
TLE epoch observation values (Epoch: 2026-06-20T03:11:29.514Z)
Latitude
-0.00001°
Longitude
-93.52166°
Altitude
483.243 km
Speed
7.625 km/s
True Right ascension
14h 50m 48s
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
21:29:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.615 km
Perigee altitude
484.367 km
Semi-major axis
6,863.128 km
Eccentricity
0.00009
Inclination
42.9991°
RAAN
222.7033°
Arg. of periapsis
227.5187°
True anomaly
132.56647°
Mean anomaly
132.5588°
Eccentric anomaly
132.56264°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.0000043306
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Other satellites on launch #160 in the year 2023 (2023-10-18 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-30551 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:31:41.210Z | 288.506° WNW | 2026-06-22 10:35:41.210Z | 88.457° E | 43.672° | 2026-06-22 10:38:41.210Z | 106.058° ESE |
| 4 mins | 2026-06-22 12:12:41.210Z | 246.892° WSW | 2026-06-22 12:13:41.210Z | 223.387° SW | 22.744° | 2026-06-22 12:16:41.210Z | 161.26° S |
| 4 mins | 2026-06-23 05:08:41.210Z | 187.432° SSW | 2026-06-23 05:10:41.210Z | 145.226° SSE | 21.353° | 2026-06-23 05:12:41.210Z | 103.541° ESE |
| 6 mins | 2026-06-23 06:46:41.210Z | 251.473° W | 2026-06-23 06:49:41.210Z | 69.014° E | 43.471° | 2026-06-23 06:52:41.210Z | 71.829° E |
| 5 mins | 2026-06-23 08:26:41.210Z | 294.937° NW | 2026-06-23 08:28:41.210Z | 14.132° NNE | 37.622° | 2026-06-23 08:31:41.210Z | 75.046° E |
| 5 mins | 2026-06-23 10:05:41.210Z | 290.849° WNW | 2026-06-23 10:07:41.210Z | 43.067° NE | 44.729° | 2026-06-23 10:10:41.210Z | 105.094° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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