STARLINK-31974, 59885
Orbit data source: Space-Track
STARLINK-31974, 59885 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 28 May 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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59885 intel report (Beta)
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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-31974
1 59885U 24100A 26036.17131090 -.00000717 00000-0 -16540-4 0 9998
2 59885 43.0019 309.0460 0001030 258.3656 101.7081 15.27589087 96088Epoch: 2026-02-05T04:06Z
TLE epoch observation values (Epoch: 2026-02-05T04:06:41.261Z)
Latitude
0.00003°
Longitude
112.04675°
Altitude
482.941 km
Speed
7.626 km/s
True Right ascension
20h 36m 11s
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
17:14:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.674 km
Perigee altitude
484.26 km
Semi-major axis
6,863.104 km
Eccentricity
0.0001
Inclination
43.0019°
RAAN
309.046°
Arg. of periapsis
258.3656°
True anomaly
101.71966°
Mean anomaly
101.7081°
Eccentric anomaly
101.71388°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
-0.00001654
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Other satellites on launch #100 in the year 2024 (2024-05-28 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-31974 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 | 2026-02-05 21:34:58.316Z | 225.899° WSW | 2026-02-05 21:37:58.316Z | 170.986° S | 35.38° | 2026-02-05 21:40:58.316Z | 83.817° E |
| 5 mins | 2026-02-05 23:14:58.316Z | 274.59° WNW | 2026-02-05 23:16:58.316Z | 327.387° NNW | 40.525° | 2026-02-05 23:19:58.316Z | 67.831° E |
| 6 mins | 2026-02-06 00:53:58.316Z | 293.47° NW | 2026-02-06 00:55:58.316Z | 334.3° NNW | 38.12° | 2026-02-06 00:59:58.316Z | 87.24° E |
| 6 mins | 2026-02-06 02:32:58.316Z | 278.321° WNW | 2026-02-06 02:34:58.316Z | 237.34° WSW | 38.035° | 2026-02-06 02:38:58.316Z | 126.968° 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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