STARLINK-30609, 58085
Orbit data source: Space-Track
STARLINK-30609, 58085 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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58085 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-30609
1 58085U 23160L 26171.40224039 .00000356 00000-0 22466-4 0 9997
2 58085 43.0038 221.2930 0001838 266.3128 93.7513 15.27577596148615Epoch: 2026-06-20T09:39Z
TLE epoch observation values (Epoch: 2026-06-20T09:39:13.569Z)
Latitude
-0.00006°
Longitude
167.86902°
Altitude
482.915 km
Speed
7.626 km/s
True Right ascension
14h 45m 10s
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
21:28:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.262 km
Perigee altitude
483.739 km
Semi-major axis
6,863.138 km
Eccentricity
0.00018
Inclination
43.0038°
RAAN
221.293°
Arg. of periapsis
266.3128°
True anomaly
93.77232°
Mean anomaly
93.7513°
Eccentric anomaly
93.76181°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.000022466
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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-30609 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 10:43:27.233Z | 287.679° WNW | 2026-06-22 10:47:27.233Z | 118.382° SE | 42.928° | 2026-06-22 10:50:27.233Z | 111.007° ESE |
| 4 mins | 2026-06-22 12:24:27.233Z | 241.61° WSW | 2026-06-22 12:25:27.233Z | 219.572° SW | 19.886° | 2026-06-22 12:28:27.233Z | 165.09° S |
| 5 mins | 2026-06-23 05:20:27.233Z | 190.781° SSW | 2026-06-23 05:22:27.233Z | 141.647° SSE | 24.539° | 2026-06-23 05:25:27.233Z | 88.383° E |
| 6 mins | 2026-06-23 06:58:27.233Z | 257.329° W | 2026-06-23 07:01:27.233Z | 51.591° ENE | 42.224° | 2026-06-23 07:04:27.233Z | 70.981° E |
| 5 mins | 2026-06-23 08:38:27.233Z | 297.91° NW | 2026-06-23 08:40:27.233Z | 20.562° NNE | 37.388° | 2026-06-23 08:43:27.233Z | 77.462° E |
| 5 mins | 2026-06-23 10:17:27.233Z | 287.527° WNW | 2026-06-23 10:19:27.233Z | 122.225° SE | 44.651° | 2026-06-23 10:22:27.233Z | 110.272° 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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