STARLINK-31270, 59154
Orbit data source: Space-Track
STARLINK-31270, 59154 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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59154 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-31270
1 59154U 24044C 26171.27473992 .00003220 00000-0 12643-3 0 9994
2 59154 43.0045 247.7729 0001089 268.7073 91.3654 15.27595539129282Epoch: 2026-06-20T06:35Z
TLE epoch observation values (Epoch: 2026-06-20T06:35:37.529Z)
Latitude
0°
Longitude
-119.62518°
Altitude
482.796 km
Speed
7.626 km/s
True Right ascension
16h 31m 05s
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
21:42:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.694 km
Perigee altitude
484.2 km
Semi-major axis
6,863.084 km
Eccentricity
0.00011
Inclination
43.0045°
RAAN
247.7729°
Arg. of periapsis
268.7073°
True anomaly
91.37788°
Mean anomaly
91.3654°
Eccentric anomaly
91.37164°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00012643
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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-31270 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 10:43:43.183Z | 287.311° WNW | 2026-06-22 10:46:43.183Z | 9.898° NNE | 37.892° | 2026-06-22 10:49:43.183Z | 76.507° E |
| 5 mins | 2026-06-22 12:23:43.183Z | 287.85° WNW | 2026-06-22 12:25:43.183Z | 196.218° SSW | 44.992° | 2026-06-22 12:28:43.183Z | 109.897° ESE |
| 4 mins | 2026-06-22 14:02:43.183Z | 249.946° W | 2026-06-22 14:04:43.183Z | 205.536° SW | 20.34° | 2026-06-22 14:06:43.183Z | 168.753° S |
| 4 mins | 2026-06-23 06:59:43.183Z | 178.77° S | 2026-06-23 07:00:43.183Z | 153.518° SSE | 23.743° | 2026-06-23 07:03:43.183Z | 92.596° ESE |
| 5 mins | 2026-06-23 08:37:43.183Z | 257.255° W | 2026-06-23 08:39:43.183Z | 8.119° NNE | 44.666° | 2026-06-23 08:42:43.183Z | 70.736° E |
| 5 mins | 2026-06-23 10:16:43.183Z | 292.923° NW | 2026-06-23 10:18:43.183Z | 354.915° N | 37.939° | 2026-06-23 10:21:43.183Z | 74.992° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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