STARLINK-31815, 59801
Orbit data source: Space-Track
STARLINK-31815, 59801 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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59801 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-31815
1 59801U 24093V 26171.47621582 -.00004022 00000-0 -13682-3 0 9996
2 59801 43.0066 348.5499 0002538 260.3192 99.7373 15.27547111118414Epoch: 2026-06-20T11:25Z
TLE epoch observation values (Epoch: 2026-06-20T11:25:45.046Z)
Latitude
-0.00004°
Longitude
-91.57813°
Altitude
483.219 km
Speed
7.625 km/s
True Right ascension
23h 14m 11s
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
00:49:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.834 km
Perigee altitude
483.35 km
Semi-major axis
6,863.229 km
Eccentricity
0.00025
Inclination
43.0066°
RAAN
348.5499°
Arg. of periapsis
260.3192°
True anomaly
99.76596°
Mean anomaly
99.7373°
Eccentric anomaly
99.75163°
Mean motion
3.81725 °/min
Orbital period
94.31 mins
BSTAR
-0.00013682
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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-31815 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 13:50:21.799Z | 185.274° SSW | 2026-06-22 13:52:21.799Z | 145.924° SSE | 19.677° | 2026-06-22 13:54:21.799Z | 105.744° ESE |
| 6 mins | 2026-06-22 15:28:21.799Z | 248.218° W | 2026-06-22 15:31:21.799Z | 84.682° E | 43.634° | 2026-06-22 15:34:21.799Z | 72.471° E |
| 5 mins | 2026-06-22 17:08:21.799Z | 293.454° NW | 2026-06-22 17:10:21.799Z | 12.046° NNE | 37.769° | 2026-06-22 17:13:21.799Z | 73.9° E |
| 5 mins | 2026-06-22 18:47:21.799Z | 292.357° WNW | 2026-06-22 18:49:21.799Z | 23.48° NE | 44.382° | 2026-06-22 18:52:21.799Z | 102.242° ESE |
| 4 mins | 2026-06-22 20:26:21.799Z | 255.112° W | 2026-06-22 20:28:21.799Z | 203.293° SW | 25.273° | 2026-06-22 20:30:21.799Z | 160.955° S |
| 4 mins | 2026-06-23 13:23:21.799Z | 173.775° S | 2026-06-23 13:24:21.799Z | 153.134° SSE | 18.997° | 2026-06-23 13:27:21.799Z | 97.561° 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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