STARLINK-31956, 59930
Orbit data source: Space-Track
STARLINK-31956, 59930 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 Jun 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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59930 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-31956
1 59930U 24106J 26171.28381644 .00001399 00000-0 60337-4 0 9997
2 59930 43.0030 113.0962 0001011 267.5355 92.5381 15.27580007116210Epoch: 2026-06-20T06:48Z
TLE epoch observation values (Epoch: 2026-06-20T06:48:41.740Z)
Latitude
-0.00001°
Longitude
102.42162°
Altitude
482.856 km
Speed
7.626 km/s
True Right ascension
07h 32m 23s
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
21:41:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.688 km
Perigee altitude
484.3 km
Semi-major axis
6,863.131 km
Eccentricity
0.0001
Inclination
43.003°
RAAN
113.0962°
Arg. of periapsis
267.5355°
True anomaly
92.54967°
Mean anomaly
92.5381°
Eccentric anomaly
92.54389°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.000060337
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Other satellites on launch #106 in the year 2024 (2024-06-01 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-31956 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 21:46:08.780Z | 180.061° SSW | 2026-06-22 21:48:08.780Z | 143.082° SSE | 17.239° | 2026-06-22 21:50:08.780Z | 106.465° ESE |
| 6 mins | 2026-06-22 23:24:08.780Z | 242.905° WSW | 2026-06-22 23:27:08.780Z | 97.03° ESE | 41.974° | 2026-06-22 23:30:08.780Z | 73.539° E |
| 6 mins | 2026-06-23 01:03:08.780Z | 283.566° WNW | 2026-06-23 01:06:08.780Z | 21° NNE | 37.302° | 2026-06-23 01:09:08.780Z | 73.335° E |
| 5 mins | 2026-06-23 02:43:08.780Z | 295.111° NW | 2026-06-23 02:45:08.780Z | 42.178° NE | 43.227° | 2026-06-23 02:48:08.780Z | 98.692° ESE |
| 4 mins | 2026-06-23 04:22:08.780Z | 255.954° W | 2026-06-23 04:24:08.780Z | 196.904° SSW | 27.804° | 2026-06-23 04:26:08.780Z | 154.451° 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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