STARLINK-31507, 59401
Orbit data source: Space-Track
STARLINK-31507, 59401 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 05 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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59401 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-31507
1 59401U 24064D 26171.45287642 -.00001791 00000-0 -55581-4 0 9998
2 59401 43.0033 195.6837 0001046 251.7381 108.3357 15.27583845124889Epoch: 2026-06-20T10:52Z
TLE epoch observation values (Epoch: 2026-06-20T10:52:08.522Z)
Latitude
-0.00002°
Longitude
123.98088°
Altitude
483.039 km
Speed
7.626 km/s
True Right ascension
13h 02m 44s
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
21:27:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.7 km
Perigee altitude
484.264 km
Semi-major axis
6,863.119 km
Eccentricity
0.0001
Inclination
43.0033°
RAAN
195.6837°
Arg. of periapsis
251.7381°
True anomaly
108.34708°
Mean anomaly
108.3357°
Eccentric anomaly
108.34139°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
-0.000055581
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Other satellites on launch #64 in the year 2024 (2024-04-05 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-31507 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 | 2026-06-22 10:26:59.898Z | 265.568° W | 2026-06-22 10:29:59.898Z | 198.74° SSW | 24.127° | 2026-06-22 10:31:59.898Z | 160.156° S |
| 4 mins | 2026-06-23 03:24:59.898Z | 170.814° S | 2026-06-23 03:25:59.898Z | 148.676° SSE | 19.794° | 2026-06-23 03:28:59.898Z | 94.892° ESE |
| 5 mins | 2026-06-23 05:02:59.898Z | 247.927° W | 2026-06-23 05:04:59.898Z | 88.571° E | 44.339° | 2026-06-23 05:07:59.898Z | 72.426° E |
| 5 mins | 2026-06-23 06:41:59.898Z | 292.264° WNW | 2026-06-23 06:43:59.898Z | 5.19° NNE | 37.996° | 2026-06-23 06:46:59.898Z | 73.508° E |
| 5 mins | 2026-06-23 08:20:59.898Z | 291.832° WNW | 2026-06-23 08:22:59.898Z | 357.991° N | 44.387° | 2026-06-23 08:25:59.898Z | 102.411° ESE |
| 5 mins | 2026-06-23 09:59:59.898Z | 256.435° W | 2026-06-23 10:01:59.898Z | 206.321° SW | 25.144° | 2026-06-23 10:04:59.898Z | 152.437° SSE |
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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