STARLINK-5942, 56014
Orbit data source: Space-Track
STARLINK-5942, 56014 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 24 Mar 2023 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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56014 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-5942
1 56014U 23042AE 26171.32859639 -.00000338 00000-0 -27550-5 0 9999
2 56014 43.0019 185.5095 0001273 265.9094 94.1612 15.27573979178730Epoch: 2026-06-20T07:53Z
TLE epoch observation values (Epoch: 2026-06-20T07:53:10.728Z)
Latitude
-0.00001°
Longitude
158.66999°
Altitude
482.906 km
Speed
7.626 km/s
True Right ascension
12h 22m 02s
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
21:24:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.886 km
Perigee altitude
484.138 km
Semi-major axis
6,863.149 km
Eccentricity
0.00013
Inclination
43.0019°
RAAN
185.5095°
Arg. of periapsis
265.9094°
True anomaly
94.17575°
Mean anomaly
94.1612°
Eccentric anomaly
94.16847°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
-0.000002755
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Other satellites on launch #42 in the year 2023 (2023-03-24 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-5942 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 | 2026-06-23 03:36:16.984Z | 212.625° SW | 2026-06-23 03:38:16.984Z | 131.845° SE | 35.782° | 2026-06-23 03:41:16.984Z | 79.419° E |
| 6 mins | 2026-06-23 05:14:16.984Z | 273.545° WNW | 2026-06-23 05:17:16.984Z | 25.103° NE | 39.229° | 2026-06-23 05:20:16.984Z | 70.55° E |
| 5 mins | 2026-06-23 06:54:16.984Z | 299.331° NW | 2026-06-23 06:56:16.984Z | 25.62° NE | 39.705° | 2026-06-23 06:59:16.984Z | 86.746° E |
| 5 mins | 2026-06-23 08:33:16.984Z | 271.496° WNW | 2026-06-23 08:35:16.984Z | 188.178° SSW | 38.701° | 2026-06-23 08:38:16.984Z | 129.091° SE |
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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