STARLINK-31704, 59586
Orbit data source: Space-Track
STARLINK-31704, 59586 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 23 Apr 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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59586 intel report (Beta)
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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 STARLINK-31704
1 59586U 24076Y 25289.16670139 .00048509 00000-0 17609-2 0 9992
2 59586 43.0009 61.6835 0001300 267.3570 242.7883 15.27576861 5911Epoch: 2025-10-16T04:00Z
TLE epoch observation values (Epoch: 2025-10-16T04:00:03.000Z)
Latitude
19.91688°
Longitude
134.01062°
Altitude
482.805 km
Speed
7.627 km/s
True Right ascension
14h 35m 48s
True Declination
19° 48' 09"
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
05:59:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.896 km
Perigee altitude
484.111 km
Semi-major axis
6,863.141 km
Eccentricity
0.00013
Inclination
43.0009°
RAAN
61.6835°
Arg. of periapsis
267.357°
True anomaly
242.77505°
Mean anomaly
242.7883°
Eccentric anomaly
242.78168°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.0017609
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Other satellites on launch #76 in the year 2024 (2024-04-23 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-31704 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 | 2025-10-16 13:00:49.770Z | 230.617° WSW | 2025-10-16 13:02:49.770Z | 139.23° SSE | 41.851° | 2025-10-16 13:05:49.770Z | 76.301° E |
| 5 mins | 2025-10-16 14:39:49.770Z | 286.068° WNW | 2025-10-16 14:41:49.770Z | 3.568° NNE | 39.013° | 2025-10-16 14:44:49.770Z | 70.7° E |
| 5 mins | 2025-10-16 16:18:49.770Z | 295.449° NW | 2025-10-16 16:20:49.770Z | 3.145° NNE | 42.092° | 2025-10-16 16:23:49.770Z | 92.545° ESE |
| 5 mins | 2025-10-16 17:57:49.770Z | 265.955° W | 2025-10-16 17:59:49.770Z | 206.266° SW | 32.876° | 2025-10-16 18:02:49.770Z | 140.933° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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