STARLINK-6237, 57055
Orbit data source: Space-Track
STARLINK-6237, 57055 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 22 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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57055 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
11.087 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-6237
1 57055U 23088H 26171.27425716 -.00000409 00000-0 -53442-5 0 9992
2 57055 43.0031 251.1296 0001885 309.5443 50.5242 15.27578034166026Epoch: 2026-06-20T06:34Z
TLE epoch observation values (Epoch: 2026-06-20T06:34:55.818Z)
Latitude
-0.00002°
Longitude
-116.09423°
Altitude
482.009 km
Speed
7.627 km/s
True Right ascension
16h 44m 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
21:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.293 km
Perigee altitude
483.706 km
Semi-major axis
6,863.137 km
Eccentricity
0.00019
Inclination
43.0031°
RAAN
251.1296°
Arg. of periapsis
309.5443°
True anomaly
50.54088°
Mean anomaly
50.5242°
Eccentric anomaly
50.53254°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
-0.0000053442
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Other satellites on launch #88 in the year 2023 (2023-06-22 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-6237 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 10:42:06.022Z | 283.388° WNW | 2026-06-22 10:45:06.022Z | 352.286° N | 37.985° | 2026-06-22 10:48:06.022Z | 72.682° E |
| 6 mins | 2026-06-22 12:22:06.022Z | 291.016° WNW | 2026-06-22 12:24:06.022Z | 323.04° NNW | 43.751° | 2026-06-22 12:28:06.022Z | 104.031° ESE |
| 5 mins | 2026-06-22 14:01:06.022Z | 258.875° W | 2026-06-22 14:03:06.022Z | 212.284° SW | 24.844° | 2026-06-22 14:06:06.022Z | 154.709° SSE |
| 4 mins | 2026-06-23 06:58:06.022Z | 178.997° S | 2026-06-23 07:00:06.022Z | 135.791° SSE | 19.466° | 2026-06-23 07:02:06.022Z | 99.983° ESE |
| 5 mins | 2026-06-23 08:36:06.022Z | 248.198° W | 2026-06-23 08:38:06.022Z | 231.741° WSW | 44.322° | 2026-06-23 08:41:06.022Z | 72.611° E |
| 6 mins | 2026-06-23 10:15:06.022Z | 287.772° WNW | 2026-06-23 10:17:06.022Z | 335.89° NNW | 37.171° | 2026-06-23 10:21:06.022Z | 75.824° 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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