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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-31815
1 59801U 24093V 26229.14704735 .00005418 00000-0 20646-3 0 9992
2 59801 43.0042 22.8584 0001073 260.5296 99.5434 15.27549164127231Epoch: 2026-08-17T03:31Z
TLE epoch observation values (Epoch: 2026-08-17T03:31:44.891Z)
Latitude
-0.00003°
Longitude
4.38793°
Altitude
483.039 km
Speed
7.626 km/s
True Right ascension
01h 31m 26s
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
03:30:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.822 km
Perigee altitude
484.349 km
Semi-major axis
6,863.223 km
Eccentricity
0.00011
Inclination
43.0042°
RAAN
22.8584°
Arg. of periapsis
260.5296°
True anomaly
99.55553°
Mean anomaly
99.5434°
Eccentric anomaly
99.54946°
Mean motion
3.81725 °/min
Orbital period
94.31 mins
BSTAR
0.00020646
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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 | 2026-08-17 13:08:26.608Z | 185.459° SSW | 2026-08-17 13:10:26.608Z | 144.185° SSE | 20.453° | 2026-08-17 13:12:26.608Z | 103.885° ESE |
| 6 mins | 2026-08-17 14:46:26.608Z | 249.771° W | 2026-08-17 14:49:26.608Z | 76.02° E | 43.111° | 2026-08-17 14:52:26.608Z | 72.143° E |
| 5 mins | 2026-08-17 16:26:26.608Z | 294.965° NW | 2026-08-17 16:28:26.608Z | 16.639° NNE | 37.461° | 2026-08-17 16:31:26.608Z | 74.701° E |
| 5 mins | 2026-08-17 18:05:26.608Z | 291.867° WNW | 2026-08-17 18:07:26.608Z | 46.298° ENE | 44.464° | 2026-08-17 18:10:26.608Z | 103.663° ESE |
| 4 mins | 2026-08-17 19:44:26.608Z | 252.667° W | 2026-08-17 19:46:26.608Z | 201.262° SSW | 24.158° | 2026-08-17 19:48:26.608Z | 161.408° S |
| 4 mins | 2026-08-18 12:41:26.608Z | 172.838° S | 2026-08-18 12:42:26.608Z | 151.002° SSE | 19.883° | 2026-08-18 12:45:26.608Z | 95.709° 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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