STARLINK-31799, 59652
Orbit data source: Space-Track
STARLINK-31799, 59652 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 03 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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59652 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-31799
1 59652U 24082X 26171.33745704 .00000161 00000-0 15357-4 0 9996
2 59652 43.0013 269.4369 0001238 242.6881 117.3845 15.27579431120684Epoch: 2026-06-20T08:05Z
TLE epoch observation values (Epoch: 2026-06-20T08:05:56.288Z)
Latitude
0.00001°
Longitude
-120.60114°
Altitude
483.217 km
Speed
7.625 km/s
True Right ascension
17h 57m 44s
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
21:23:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.845 km
Perigee altitude
484.146 km
Semi-major axis
6,863.133 km
Eccentricity
0.00012
Inclination
43.0013°
RAAN
269.4369°
Arg. of periapsis
242.6881°
True anomaly
117.3971°
Mean anomaly
117.3845°
Eccentric anomaly
117.3908°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.000015357
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Other satellites on launch #82 in the year 2024 (2024-05-03 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-31799 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 10:34:25.647Z | 257.215° W | 2026-06-22 10:38:25.647Z | 46.299° ENE | 42.242° | 2026-06-22 10:41:25.647Z | 70.776° E |
| 5 mins | 2026-06-22 12:15:25.647Z | 297.944° NW | 2026-06-22 12:17:25.647Z | 19.432° NNE | 37.574° | 2026-06-22 12:20:25.647Z | 78.017° E |
| 5 mins | 2026-06-22 13:54:25.647Z | 286.368° WNW | 2026-06-22 13:56:25.647Z | 142.18° SSE | 44.633° | 2026-06-22 13:59:25.647Z | 111.837° ESE |
| 4 mins | 2026-06-22 15:33:25.647Z | 246.287° WSW | 2026-06-22 15:34:25.647Z | 225.943° WSW | 19.112° | 2026-06-22 15:37:25.647Z | 168.742° S |
| 5 mins | 2026-06-23 08:29:25.647Z | 195.682° SSW | 2026-06-23 08:31:25.647Z | 150.05° SSE | 25.107° | 2026-06-23 08:34:25.647Z | 90.325° ESE |
| 5 mins | 2026-06-23 10:08:25.647Z | 260.135° W | 2026-06-23 10:10:25.647Z | 25.652° NE | 44.072° | 2026-06-23 10:13:25.647Z | 70.536° E |
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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