STARLINK-31710, 59378
Orbit data source: Space-Track
STARLINK-31710, 59378 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 02 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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59378 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-31710
1 59378U 24062E 26171.19680173 .00004452 00000-0 14285-3 0 9996
2 59378 53.1604 138.9653 0001019 95.2436 264.8683 15.34390640125334Epoch: 2026-06-20T04:43Z
TLE epoch observation values (Epoch: 2026-06-20T04:43:23.669Z)
Latitude
-0.00001°
Longitude
159.70178°
Altitude
463.695 km
Speed
7.636 km/s
True Right ascension
09h 15m 51s
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
21:27:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.685 km
Perigee altitude
462.291 km
Semi-major axis
6,841.125 km
Eccentricity
0.0001
Inclination
53.1604°
RAAN
138.9653°
Arg. of periapsis
95.2436°
True anomaly
264.85667°
Mean anomaly
264.8683°
Eccentric anomaly
264.86249°
Mean motion
3.83576 °/min
Orbital period
93.85 mins
BSTAR
0.00014285
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Other satellites on launch #62 in the year 2024 (2024-04-02 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-31710 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 | 2026-06-23 00:08:39.179Z | 244.511° WSW | 2026-06-23 00:10:39.179Z | 283.847° WNW | 39.687° | 2026-06-23 00:13:39.179Z | 40.987° NE |
| 4 mins | 2026-06-23 05:05:39.179Z | 354.255° N | 2026-06-23 05:06:39.179Z | 15.035° NNE | 18.009° | 2026-06-23 05:09:39.179Z | 71.287° E |
| 5 mins | 2026-06-23 06:42:39.179Z | 305.767° NW | 2026-06-23 06:44:39.179Z | 278.802° WNW | 42.807° | 2026-06-23 06:47:39.179Z | 137.007° 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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