STARLINK-31970, 59928
Orbit data source: Space-Track
STARLINK-31970, 59928 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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59928 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: 1 day ago
TLE from 1 day ago
0 STARLINK-31970
1 59928U 24106G 26261.19660822 -.00000075 00000-0 68144-5 0 9998
2 59928 43.0030 325.4004 0001801 285.0509 75.0143 15.27570952130010Epoch: 2026-09-18T04:43Z
TLE epoch observation values (Epoch: 2026-09-18T04:43:06.950Z)
Latitude
-0.00003°
Longitude
-102.50155°
Altitude
482.533 km
Speed
7.626 km/s
True Right ascension
21h 41m 36s
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
22:07:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.257 km
Perigee altitude
483.785 km
Semi-major axis
6,863.158 km
Eccentricity
0.00018
Inclination
43.003°
RAAN
325.4004°
Arg. of periapsis
285.0509°
True anomaly
75.03424°
Mean anomaly
75.0143°
Eccentric anomaly
75.02427°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
0.0000068144
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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-31970 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 | 2026-09-19 07:36:34.380Z | 219.531° SW | 2026-09-19 07:39:34.380Z | 141.758° SSE | 42.684° | 2026-09-19 07:42:34.380Z | 81.732° E |
| 6 mins | 2026-09-19 09:15:34.380Z | 270.111° WNW | 2026-09-19 09:18:34.380Z | 16.796° NNE | 59.518° | 2026-09-19 09:21:34.380Z | 69.487° E |
| 5 mins | 2026-09-19 10:55:34.380Z | 298.457° NW | 2026-09-19 10:57:34.380Z | 12.601° NNE | 54.461° | 2026-09-19 11:00:34.380Z | 83.144° E |
| 5 mins | 2026-09-19 12:34:34.380Z | 277.557° WNW | 2026-09-19 12:36:34.380Z | 198.466° SSW | 62.831° | 2026-09-19 12:39:34.380Z | 124.747° 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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