STARLINK-32105, 59689
Orbit data source: Space-Track
STARLINK-32105, 59689 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 08 May 2024 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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59689 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-32105
1 59689U 24086H 26171.13958078 .00000424 00000-0 24925-4 0 9991
2 59689 43.0025 201.0514 0001670 275.3475 84.7186 15.27577716119781Epoch: 2026-06-20T03:20Z
TLE epoch observation values (Epoch: 2026-06-20T03:20:59.779Z)
Latitude
-0.00002°
Longitude
-117.55619°
Altitude
482.726 km
Speed
7.626 km/s
True Right ascension
13h 24m 12s
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
21:32:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.147 km
Perigee altitude
483.855 km
Semi-major axis
6,863.138 km
Eccentricity
0.00017
Inclination
43.0025°
RAAN
201.0514°
Arg. of periapsis
275.3475°
True anomaly
84.73766°
Mean anomaly
84.7186°
Eccentric anomaly
84.72813°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.000024925
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Other satellites on launch #86 in the year 2024 (2024-05-08 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-32105 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 10:46:55.504Z | 263.758° W | 2026-06-22 10:48:55.504Z | 226.81° WSW | 22.441° | 2026-06-22 10:51:55.504Z | 162.796° S |
| 4 mins | 2026-06-23 03:44:55.504Z | 172.286° S | 2026-06-23 03:45:55.504Z | 148.515° SSE | 21.406° | 2026-06-23 03:48:55.504Z | 93.256° ESE |
| 5 mins | 2026-06-23 05:22:55.504Z | 251.998° W | 2026-06-23 05:24:55.504Z | 66.491° ENE | 44.325° | 2026-06-23 05:27:55.504Z | 71.75° E |
| 5 mins | 2026-06-23 07:01:55.504Z | 293.425° NW | 2026-06-23 07:03:55.504Z | 5.914° NNE | 37.932° | 2026-06-23 07:06:55.504Z | 74.445° E |
| 5 mins | 2026-06-23 08:40:55.504Z | 290.536° WNW | 2026-06-23 08:42:55.504Z | 352.246° N | 44.745° | 2026-06-23 08:45:55.504Z | 105.062° ESE |
| 4 mins | 2026-06-23 10:19:55.504Z | 254.251° W | 2026-06-23 10:21:55.504Z | 206.39° SW | 23.386° | 2026-06-23 10:23:55.504Z | 165.124° S |
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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