STARLINK-31106, 58689
Orbit data source: Space-Track
STARLINK-31106, 58689 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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58689 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-31106
1 58689U 23211Y 26171.20952510 .00008765 00000-0 32752-3 0 9994
2 58689 43.0022 226.3062 0001563 269.2308 90.8365 15.27592832138147Epoch: 2026-06-20T05:01Z
TLE epoch observation values (Epoch: 2026-06-20T05:01:42.968Z)
Latitude
0°
Longitude
-117.55026°
Altitude
482.802 km
Speed
7.626 km/s
True Right ascension
15h 05m 13s
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
21:28:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.028 km
Perigee altitude
483.883 km
Semi-major axis
6,863.092 km
Eccentricity
0.00016
Inclination
43.0022°
RAAN
226.3062°
Arg. of periapsis
269.2308°
True anomaly
90.85441°
Mean anomaly
90.8365°
Eccentric anomaly
90.84545°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00032752
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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-31106 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 10:48:21.190Z | 289.003° WNW | 2026-06-22 10:51:21.190Z | 7.255° NNE | 44.854° | 2026-06-22 10:54:21.190Z | 105.838° ESE |
| 4 mins | 2026-06-22 12:28:21.190Z | 252.966° W | 2026-06-22 12:30:21.190Z | 205.232° SW | 22.841° | 2026-06-22 12:32:21.190Z | 165.256° S |
| 4 mins | 2026-06-23 05:25:21.190Z | 175.66° S | 2026-06-23 05:26:21.190Z | 152.87° SSE | 21.218° | 2026-06-23 05:29:21.190Z | 94.989° ESE |
| 5 mins | 2026-06-23 07:03:21.190Z | 251.814° W | 2026-06-23 07:05:21.190Z | 57.261° ENE | 44.929° | 2026-06-23 07:08:21.190Z | 71.72° E |
| 5 mins | 2026-06-23 08:42:21.190Z | 291.641° WNW | 2026-06-23 08:44:21.190Z | 355.257° N | 37.975° | 2026-06-23 08:47:21.190Z | 73.571° E |
| 5 mins | 2026-06-23 10:21:21.190Z | 290.275° WNW | 2026-06-23 10:23:21.190Z | 319.071° NNW | 44.238° | 2026-06-23 10:26:21.190Z | 104.817° 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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