STARLINK-31327, 59160
Orbit data source: Space-Track
STARLINK-31327, 59160 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 04 Mar 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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59160 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-31327
1 59160U 24044J 26171.47734483 -.00001427 00000-0 -42314-4 0 9996
2 59160 43.0028 246.7116 0001633 270.6272 89.4393 15.27583820129319Epoch: 2026-06-20T11:27Z
TLE epoch observation values (Epoch: 2026-06-20T11:27:22.593Z)
Latitude
0.00002°
Longitude
166.17608°
Altitude
482.803 km
Speed
7.626 km/s
True Right ascension
16h 26m 50s
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
23:27:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.103 km
Perigee altitude
483.862 km
Semi-major axis
6,863.119 km
Eccentricity
0.00016
Inclination
43.0028°
RAAN
246.7116°
Arg. of periapsis
270.6272°
True anomaly
89.45801°
Mean anomaly
89.4393°
Eccentric anomaly
89.44866°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
-0.000042314
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Other satellites on launch #44 in the year 2024 (2024-03-04 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-31327 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 12:32:45.727Z | 286.162° WNW | 2026-06-22 12:35:45.727Z | 146.861° SSE | 43.841° | 2026-06-22 12:38:45.727Z | 114.328° SE |
| 4 mins | 2026-06-22 14:12:45.727Z | 243.038° WSW | 2026-06-22 14:13:45.727Z | 222.988° SW | 17.946° | 2026-06-22 14:16:45.727Z | 169.738° S |
| 5 mins | 2026-06-23 07:08:45.727Z | 196.9° SSW | 2026-06-23 07:10:45.727Z | 146.688° SSE | 26.783° | 2026-06-23 07:13:45.727Z | 88.011° E |
| 6 mins | 2026-06-23 08:46:45.727Z | 260.255° W | 2026-06-23 08:49:45.727Z | 29.913° NE | 43.157° | 2026-06-23 08:52:45.727Z | 70.328° E |
| 5 mins | 2026-06-23 10:26:45.727Z | 296.363° NW | 2026-06-23 10:28:45.727Z | 9.525° NNE | 38.132° | 2026-06-23 10:31:45.727Z | 78.021° E |
| 5 mins | 2026-06-23 12:05:45.727Z | 285.388° WNW | 2026-06-23 12:07:45.727Z | 202.106° SSW | 44.704° | 2026-06-23 12:10:45.727Z | 113.74° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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