STARLINK-5869, 57061
Orbit data source: Space-Track
STARLINK-5869, 57061 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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57061 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-5869
1 57061U 23088P 26171.21223909 .00000550 00000-0 29497-4 0 9990
2 57061 43.0039 254.9207 0001314 266.0819 93.9882 15.27575197164997Epoch: 2026-06-20T05:05Z
TLE epoch observation values (Epoch: 2026-06-20T05:05:37.457Z)
Latitude
-0.00005°
Longitude
-89.91553°
Altitude
482.902 km
Speed
7.626 km/s
True Right ascension
16h 59m 40s
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
21:33:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.91 km
Perigee altitude
484.106 km
Semi-major axis
6,863.145 km
Eccentricity
0.00013
Inclination
43.0039°
RAAN
254.9207°
Arg. of periapsis
266.0819°
True anomaly
94.00322°
Mean anomaly
93.9882°
Eccentric anomaly
93.99571°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.000029497
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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-5869 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 10:46:40.928Z | 282.422° WNW | 2026-06-22 10:49:40.928Z | 3.632° NNE | 38.218° | 2026-06-22 10:52:40.928Z | 72.359° E |
| 5 mins | 2026-06-22 12:26:40.928Z | 293.238° NW | 2026-06-22 12:28:40.928Z | 358.954° N | 43.721° | 2026-06-22 12:31:40.928Z | 99.011° ESE |
| 5 mins | 2026-06-22 14:05:40.928Z | 259.618° W | 2026-06-22 14:07:40.928Z | 206.705° SW | 27.602° | 2026-06-22 14:10:40.928Z | 149.005° SSE |
| 4 mins | 2026-06-23 07:02:40.928Z | 173.217° S | 2026-06-23 07:04:40.928Z | 133.15° SE | 17.032° | 2026-06-23 07:06:40.928Z | 100.438° ESE |
| 5 mins | 2026-06-23 08:40:40.928Z | 242.128° WSW | 2026-06-23 08:42:40.928Z | 174.2° S | 44.298° | 2026-06-23 08:45:40.928Z | 74.087° E |
| 5 mins | 2026-06-23 10:19:40.928Z | 287.338° WNW | 2026-06-23 10:21:40.928Z | 346.001° N | 38.171° | 2026-06-23 10:24:40.928Z | 70.779° 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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