STARLINK-6223, 57057
Orbit data source: Space-Track
STARLINK-6223, 57057 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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57057 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: 3 days ago
TLE from 3 days ago
0 STARLINK-6223
1 57057U 23088K 26170.68320567 .00000706 00000-0 35172-4 0 9993
2 57057 43.0039 254.4091 0001535 281.4007 78.6672 15.27573951165931Epoch: 2026-06-19T16:23Z
TLE epoch observation values (Epoch: 2026-06-19T16:23:48.969Z)
Latitude
-0.00005°
Longitude
100.54634°
Altitude
482.636 km
Speed
7.626 km/s
True Right ascension
16h 57m 38s
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
21:31:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.065 km
Perigee altitude
483.958 km
Semi-major axis
6,863.149 km
Eccentricity
0.00015
Inclination
43.0039°
RAAN
254.4091°
Arg. of periapsis
281.4007°
True anomaly
78.68445°
Mean anomaly
78.6672°
Eccentric anomaly
78.67582°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.000035172
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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-6223 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 10:38:35.478Z | 284.763° WNW | 2026-06-22 10:41:35.478Z | 16.375° NNE | 37.522° | 2026-06-22 10:44:35.478Z | 74.024° E |
| 5 mins | 2026-06-22 12:18:35.478Z | 292.968° NW | 2026-06-22 12:20:35.478Z | 38.497° NE | 44.158° | 2026-06-22 12:23:35.478Z | 101.733° ESE |
| 4 mins | 2026-06-22 13:57:35.478Z | 254.322° W | 2026-06-22 13:59:35.478Z | 200.714° SSW | 25.557° | 2026-06-22 14:01:35.478Z | 159.282° S |
| 4 mins | 2026-06-23 06:54:35.478Z | 171.318° S | 2026-06-23 06:55:35.478Z | 150.504° SSE | 18.67° | 2026-06-23 06:58:35.478Z | 96.782° ESE |
| 5 mins | 2026-06-23 08:32:35.478Z | 245.316° WSW | 2026-06-23 08:34:35.478Z | 114.837° SE | 44.539° | 2026-06-23 08:37:35.478Z | 72.988° E |
| 5 mins | 2026-06-23 10:11:35.478Z | 290.551° WNW | 2026-06-23 10:13:35.478Z | 359.634° N | 38.164° | 2026-06-23 10:16:35.478Z | 72.541° 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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