STARLINK-30598, 58079
Orbit data source: Space-Track
STARLINK-30598, 58079 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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58079 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-30598
1 58079U 23160E 26171.39502323 -.00002787 00000-0 -91739-4 0 9994
2 58079 43.0039 217.8364 0001776 267.1127 92.9522 15.27589576148656Epoch: 2026-06-20T09:28Z
TLE epoch observation values (Epoch: 2026-06-20T09:28:50.007Z)
Latitude
0.00004°
Longitude
167.01781°
Altitude
482.859 km
Speed
7.626 km/s
True Right ascension
14h 31m 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
21:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.184 km
Perigee altitude
483.746 km
Semi-major axis
6,863.102 km
Eccentricity
0.00018
Inclination
43.0039°
RAAN
217.8364°
Arg. of periapsis
267.1127°
True anomaly
92.97252°
Mean anomaly
92.9522°
Eccentric anomaly
92.96236°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
-0.000091739
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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-30598 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 10:33:51.409Z | 286.987° WNW | 2026-06-22 10:36:51.409Z | 172.162° S | 44.758° | 2026-06-22 10:39:51.409Z | 112.787° SE |
| 4 mins | 2026-06-22 12:13:51.409Z | 247.203° WSW | 2026-06-22 12:15:51.409Z | 204.744° SW | 18.631° | 2026-06-22 12:17:51.409Z | 170.477° S |
| 5 mins | 2026-06-23 05:09:51.409Z | 197.768° SSW | 2026-06-23 05:11:51.409Z | 152.762° SSE | 25.643° | 2026-06-23 05:14:51.409Z | 90.563° ESE |
| 5 mins | 2026-06-23 06:48:51.409Z | 260.963° W | 2026-06-23 06:50:51.409Z | 7.362° NNE | 44.219° | 2026-06-23 06:53:51.409Z | 70.243° E |
| 5 mins | 2026-06-23 08:27:51.409Z | 293.982° NW | 2026-06-23 08:29:51.409Z | 356.874° N | 38.072° | 2026-06-23 08:32:51.409Z | 76.311° E |
| 5 mins | 2026-06-23 10:06:51.409Z | 286.735° WNW | 2026-06-23 10:08:51.409Z | 262.959° W | 44.442° | 2026-06-23 10:11:51.409Z | 112.104° 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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