STARLINK-31608, 59397
Orbit data source: Space-Track
STARLINK-31608, 59397 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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59397 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-31608
1 59397U 24062X 26171.17794195 .00000701 00000-0 31886-4 0 9995
2 59397 53.1613 139.5565 0001323 88.0562 272.0592 15.34392871125318Epoch: 2026-06-20T04:16Z
TLE epoch observation values (Epoch: 2026-06-20T04:16:14.184Z)
Latitude
-0.00003°
Longitude
167.10108°
Altitude
463.594 km
Speed
7.636 km/s
True Right ascension
09h 18m 13s
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
23:07:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.886 km
Perigee altitude
462.076 km
Semi-major axis
6,841.118 km
Eccentricity
0.00013
Inclination
53.1613°
RAAN
139.5565°
Arg. of periapsis
88.0562°
True anomaly
272.04405°
Mean anomaly
272.0592°
Eccentric anomaly
272.05162°
Mean motion
3.83577 °/min
Orbital period
93.85 mins
BSTAR
0.000031886
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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-31608 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 | 2026-06-22 23:40:09.326Z | 217.241° SW | 2026-06-22 23:43:09.326Z | 96.917° ESE | 41.004° | 2026-06-22 23:46:09.326Z | 55.249° ENE |
| 4 mins | 2026-06-23 01:19:09.326Z | 301.187° NW | 2026-06-23 01:21:09.326Z | 346.284° N | 19.067° | 2026-06-23 01:23:09.326Z | 22.302° NNE |
| 5 mins | 2026-06-23 06:15:09.326Z | 332.032° NNW | 2026-06-23 06:17:09.326Z | 69.152° E | 37.187° | 2026-06-23 06:20:09.326Z | 115.189° 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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