STARLINK-31128, 58669
Orbit data source: Space-Track
STARLINK-31128, 58669 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 29 Dec 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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58669 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-31128
1 58669U 23211C 26171.20309934 -.00000218 00000-0 15969-5 0 9997
2 58669 43.0025 226.2566 0001169 268.6410 91.4308 15.27575320138142Epoch: 2026-06-20T04:52Z
TLE epoch observation values (Epoch: 2026-06-20T04:52:27.782Z)
Latitude
-0.00002°
Longitude
-115.28028°
Altitude
482.859 km
Speed
7.626 km/s
True Right ascension
15h 05m 01s
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
21:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.81 km
Perigee altitude
484.206 km
Semi-major axis
6,863.145 km
Eccentricity
0.00012
Inclination
43.0025°
RAAN
226.2566°
Arg. of periapsis
268.641°
True anomaly
91.44419°
Mean anomaly
91.4308°
Eccentric anomaly
91.4375°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.0000015969
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Other satellites on launch #211 in the year 2023 (2023-12-29 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-31128 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 10:38:22.691Z | 289.383° WNW | 2026-06-22 10:41:22.691Z | 319.798° NNW | 42.876° | 2026-06-22 10:45:22.691Z | 102.619° ESE |
| 5 mins | 2026-06-22 12:18:22.691Z | 261.391° W | 2026-06-22 12:20:22.691Z | 215.496° SW | 25.813° | 2026-06-22 12:23:22.691Z | 153.991° SSE |
| 4 mins | 2026-06-23 05:15:22.691Z | 179.412° S | 2026-06-23 05:17:22.691Z | 138.448° SSE | 18.755° | 2026-06-23 05:19:22.691Z | 102.164° ESE |
| 6 mins | 2026-06-23 06:53:22.691Z | 246.294° WSW | 2026-06-23 06:55:22.691Z | 227.663° WSW | 43.553° | 2026-06-23 06:59:22.691Z | 72.682° E |
| 6 mins | 2026-06-23 08:32:22.691Z | 286.307° WNW | 2026-06-23 08:34:22.691Z | 330.055° NNW | 36.74° | 2026-06-23 08:38:22.691Z | 74.952° E |
| 6 mins | 2026-06-23 10:11:22.691Z | 290.895° WNW | 2026-06-23 10:14:22.691Z | 69.653° E | 42.703° | 2026-06-23 10:17:22.691Z | 101.593° 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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