STARLINK-31885, 59660
Orbit data source: Space-Track
STARLINK-31885, 59660 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 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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59660 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: 5 hours ago
TLE from 5 hours ago
0 STARLINK-31885
1 59660U 24084G 26073.53453882 .00001829 00000-0 75951-4 0 9991
2 59660 43.0040 11.0188 0000566 250.6868 109.3923 15.27588664105151Epoch: 2026-03-14T12:49Z
TLE epoch observation values (Epoch: 2026-03-14T12:49:44.154Z)
Latitude
0.00003°
Longitude
6.43053°
Altitude
482.928 km
Speed
7.626 km/s
True Right ascension
00h 44m 04s
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
22:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.356 km
Perigee altitude
484.579 km
Semi-major axis
6,863.105 km
Eccentricity
0.00006
Inclination
43.004°
RAAN
11.0188°
Arg. of periapsis
250.6868°
True anomaly
109.39842°
Mean anomaly
109.3923°
Eccentric anomaly
109.39536°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000075951
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Other satellites on launch #84 in the year 2024 (2024-05-06 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-31885 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 | 2026-03-14 22:25:37.675Z | 187.153° SSW | 2026-03-14 22:27:37.675Z | 152.754° SSE | 17.944° | 2026-03-14 22:30:37.675Z | 98.553° ESE |
| 5 mins | 2026-03-15 00:04:37.675Z | 243.978° WSW | 2026-03-15 00:06:37.675Z | 149.467° SSE | 44.605° | 2026-03-15 00:09:37.675Z | 73.43° E |
| 5 mins | 2026-03-15 01:43:37.675Z | 288.953° WNW | 2026-03-15 01:45:37.675Z | 352.467° N | 38.195° | 2026-03-15 01:48:37.675Z | 71.684° E |
| 5 mins | 2026-03-15 03:22:37.675Z | 292.349° WNW | 2026-03-15 03:24:37.675Z | 334.962° NNW | 43.234° | 2026-03-15 03:27:37.675Z | 99.254° ESE |
| 5 mins | 2026-03-15 05:01:37.675Z | 261.435° W | 2026-03-15 05:03:37.675Z | 212.24° SW | 27.173° | 2026-03-15 05:06:37.675Z | 150.991° 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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