STARLINK-31810, 59799
Orbit data source: Space-Track
STARLINK-31810, 59799 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 18 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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59799 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-31810
1 59799U 24093T 26171.48006728 -.00002453 00000-0 -79684-4 0 9993
2 59799 43.0028 348.5789 0000842 257.2456 102.8302 15.27560287118411Epoch: 2026-06-20T11:31Z
TLE epoch observation values (Epoch: 2026-06-20T11:31:17.812Z)
Latitude
0.00003°
Longitude
-92.93938°
Altitude
483.012 km
Speed
7.626 km/s
True Right ascension
23h 14m 18s
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
00:51:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.631 km
Perigee altitude
484.475 km
Semi-major axis
6,863.19 km
Eccentricity
0.00008
Inclination
43.0028°
RAAN
348.5789°
Arg. of periapsis
257.2456°
True anomaly
102.83961°
Mean anomaly
102.8302°
Eccentric anomaly
102.8349°
Mean motion
3.81728 °/min
Orbital period
94.31 mins
BSTAR
-0.000079684
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Other satellites on launch #93 in the year 2024 (2024-05-18 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-31810 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 13:55:35.300Z | 194.542° SSW | 2026-06-22 13:58:35.300Z | 134.712° SE | 20.768° | 2026-06-22 14:00:35.300Z | 98.337° ESE |
| 5 mins | 2026-06-22 15:34:35.300Z | 251.235° W | 2026-06-22 15:36:35.300Z | 253.173° W | 44.469° | 2026-06-22 15:39:35.300Z | 71.753° E |
| 6 mins | 2026-06-22 17:13:35.300Z | 288.813° WNW | 2026-06-22 17:15:35.300Z | 336.81° NNW | 37.087° | 2026-06-22 17:19:35.300Z | 76.665° E |
| 6 mins | 2026-06-22 18:52:35.300Z | 289.929° WNW | 2026-06-22 18:55:35.300Z | 89.874° E | 42.293° | 2026-06-22 18:58:35.300Z | 105.175° ESE |
| 4 mins | 2026-06-22 20:32:35.300Z | 244.631° WSW | 2026-06-22 20:33:35.300Z | 219.503° SW | 23.651° | 2026-06-22 20:36:35.300Z | 158.634° S |
| 4 mins | 2026-06-23 13:28:35.300Z | 184.619° SSW | 2026-06-23 13:30:35.300Z | 142.097° SSE | 20.674° | 2026-06-23 13:32:35.300Z | 102.475° 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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