STARLINK-31652, 59256
Orbit data source: Space-Track
STARLINK-31652, 59256 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 19 Mar 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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59256 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-31652
1 59256U 24050C 26171.33336806 -.00020781 00000-0 -65955-3 0 9990
2 59256 53.1595 64.0095 0001066 91.3984 25.9328 15.31709848 5828Epoch: 2026-06-20T08:00Z
TLE epoch observation values (Epoch: 2026-06-20T08:00:03.000Z)
Latitude
45.45307°
Longitude
166.25305°
Altitude
474.84 km
Speed
7.634 km/s
True Right ascension
12h 59m 15s
True Declination
45° 16' 26"
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
21:27:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.697 km
Perigee altitude
470.237 km
Semi-major axis
6,849.104 km
Eccentricity
0.00011
Inclination
53.1595°
RAAN
64.0095°
Arg. of periapsis
91.3984°
True anomaly
25.93814°
Mean anomaly
25.9328°
Eccentric anomaly
25.93547°
Mean motion
3.82906 °/min
Orbital period
94.02 mins
BSTAR
-0.00065955
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Other satellites on launch #50 in the year 2024 (2024-03-19 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-31652 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 19:12:05.181Z | 241.264° WSW | 2026-06-22 19:14:05.181Z | 282.624° WNW | 41.779° | 2026-06-22 19:17:05.181Z | 43.387° NE |
| 4 mins | 2026-06-23 00:09:05.181Z | 347° N | 2026-06-23 00:11:05.181Z | 27.224° NE | 17.861° | 2026-06-23 00:13:05.181Z | 64.266° ENE |
| 5 mins | 2026-06-23 01:47:05.181Z | 307.55° NW | 2026-06-23 01:49:05.181Z | 230.785° WSW | 44.831° | 2026-06-23 01:52:05.181Z | 133.741° SE |
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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