STARLINK-31471, 59568
Orbit data source: Space-Track
STARLINK-31471, 59568 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 23 Apr 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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59568 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-31471
1 59568U 24076E 25257.47086562 -.00124019 00000-0 -44468-2 0 9998
2 59568 43.0021 284.0764 0001038 248.4024 111.6718 15.28494006 79462Epoch: 2025-09-14T11:18Z
TLE epoch observation values (Epoch: 2025-09-14T11:18:02.789Z)
Latitude
0.00001°
Longitude
120.87539°
Altitude
480.352 km
Speed
7.627 km/s
True Right ascension
18h 56m 18s
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
00:38:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.971 km
Perigee altitude
481.547 km
Semi-major axis
6,860.396 km
Eccentricity
0.0001
Inclination
43.0021°
RAAN
284.0764°
Arg. of periapsis
248.4024°
True anomaly
111.68285°
Mean anomaly
111.6718°
Eccentric anomaly
111.67733°
Mean motion
3.81961 °/min
Orbital period
94.25 mins
BSTAR
-0.0044468
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Other satellites on launch #76 in the year 2024 (2024-04-23 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-31471 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-15 08:01:49.184Z | 284.439° WNW | 2025-09-15 08:04:49.184Z | 334.435° NNW | 36.628° | 2025-09-15 08:08:49.184Z | 78.35° E |
| 6 mins | 2025-09-15 09:41:49.184Z | 288° WNW | 2025-09-15 09:44:49.184Z | 111.13° ESE | 42.476° | 2025-09-15 09:47:49.184Z | 109.696° ESE |
| 4 mins | 2025-09-15 11:21:49.184Z | 240.488° WSW | 2025-09-15 11:22:49.184Z | 217.367° SW | 20.652° | 2025-09-15 11:25:49.184Z | 162.831° S |
| 4 mins | 2025-09-16 04:17:49.184Z | 180.456° SSW | 2025-09-16 04:18:49.184Z | 156.245° SSE | 23.282° | 2025-09-16 04:21:49.184Z | 93.852° ESE |
| 5 mins | 2025-09-16 05:55:49.184Z | 256.514° W | 2025-09-16 05:57:49.184Z | 343.775° N | 44.774° | 2025-09-16 06:00:49.184Z | 70.77° E |
| 5 mins | 2025-09-16 07:34:49.184Z | 292.367° WNW | 2025-09-16 07:36:49.184Z | 352.231° N | 37.85° | 2025-09-16 07:39:49.184Z | 74.602° E |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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