STARLINK-31398, 59415
Orbit data source: Space-Track
STARLINK-31398, 59415 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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59415 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: 3 days ago
TLE from 3 days ago
0 STARLINK-31398
1 59415U 24064T 26170.54131101 .00000803 00000-0 38693-4 0 9996
2 59415 43.0029 200.8830 0001332 275.0192 85.0508 15.27586907124801Epoch: 2026-06-19T12:59Z
TLE epoch observation values (Epoch: 2026-06-19T12:59:29.271Z)
Latitude
0.00002°
Longitude
98.24225°
Altitude
482.725 km
Speed
7.626 km/s
True Right ascension
13h 23m 31s
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
21:24:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.887 km
Perigee altitude
484.059 km
Semi-major axis
6,863.11 km
Eccentricity
0.00013
Inclination
43.0029°
RAAN
200.883°
Arg. of periapsis
275.0192°
True anomaly
85.06601°
Mean anomaly
85.0508°
Eccentric anomaly
85.0584°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000038693
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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-31398 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 10:33:03.218Z | 260.543° W | 2026-06-22 10:35:03.218Z | 219.509° SW | 22.967° | 2026-06-22 10:38:03.218Z | 159.826° S |
| 4 mins | 2026-06-23 03:30:03.218Z | 185.199° SSW | 2026-06-23 03:32:03.218Z | 141.329° SSE | 21.299° | 2026-06-23 03:34:03.218Z | 101.443° ESE |
| 6 mins | 2026-06-23 05:08:03.218Z | 251.564° W | 2026-06-23 05:10:03.218Z | 253.661° W | 42.516° | 2026-06-23 05:14:03.218Z | 71.847° E |
| 6 mins | 2026-06-23 06:47:03.218Z | 287.004° WNW | 2026-06-23 06:50:03.218Z | 23.149° NE | 36.944° | 2026-06-23 06:53:03.218Z | 75.725° E |
| 5 mins | 2026-06-23 08:27:03.218Z | 291.248° WNW | 2026-06-23 08:29:03.218Z | 75.174° E | 44.227° | 2026-06-23 08:32:03.218Z | 105.244° ESE |
| 4 mins | 2026-06-23 10:06:03.218Z | 249.417° W | 2026-06-23 10:07:03.218Z | 226.484° WSW | 22.999° | 2026-06-23 10:10:03.218Z | 161.635° S |
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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