STARLINK-31706, 59437
Orbit data source: Space-Track
STARLINK-31706, 59437 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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59437 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-31706
1 59437U 24065S 26171.36878992 .00000667 00000-0 34649-4 0 9993
2 59437 53.1591 166.6239 0001364 70.9538 289.1610 15.30201058124620Epoch: 2026-06-20T08:51Z
TLE epoch observation values (Epoch: 2026-06-20T08:51:03.449Z)
Latitude
-0.00003°
Longitude
125.27509°
Altitude
475.805 km
Speed
7.629 km/s
True Right ascension
11h 06m 29s
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
21:27:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.403 km
Perigee altitude
474.534 km
Semi-major axis
6,853.605 km
Eccentricity
0.00014
Inclination
53.1591°
RAAN
166.6239°
Arg. of periapsis
70.9538°
True anomaly
289.14623°
Mean anomaly
289.161°
Eccentric anomaly
289.15362°
Mean motion
3.82529 °/min
Orbital period
94.11 mins
BSTAR
0.000034649
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Other satellites on launch #65 in the year 2024 (2024-04-07 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-31706 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-23 01:16:39.982Z | 210.026° SW | 2026-06-23 01:19:39.982Z | 160.699° S | 35.673° | 2026-06-23 01:22:39.982Z | 64.908° ENE |
| 4 mins | 2026-06-23 02:56:39.982Z | 295.768° NW | 2026-06-23 02:58:39.982Z | 346.179° N | 22.231° | 2026-06-23 03:00:39.982Z | 23.859° NE |
| 5 mins | 2026-06-23 07:52:39.982Z | 328.293° NNW | 2026-06-23 07:54:39.982Z | 14.178° NNE | 33.554° | 2026-06-23 07:57:39.982Z | 102.022° ESE |
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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