STARLINK-5862, 55920
Orbit data source: Space-Track
STARLINK-5862, 55920 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 17 Mar 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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55920 intel report (Beta)
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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 STARLINK-5862
1 55920U 23037G 25349.82786948 .00000539 00000-0 52935-4 0 9996
2 55920 69.9996 136.0976 0003248 269.2571 90.8216 14.98330584151415Epoch: 2025-12-15T19:52Z
TLE epoch observation values (Epoch: 2025-12-15T19:52:07.923Z)
Latitude
0.00001°
Longitude
113.34375°
Altitude
574.511 km
Speed
7.574 km/s
True Right ascension
09h 04m 23s
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
12:48:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.259 km
Perigee altitude
567.746 km
Semi-major axis
6,948.139 km
Eccentricity
0.00032
Inclination
69.9996°
RAAN
136.0976°
Arg. of periapsis
269.2571°
True anomaly
90.85882°
Mean anomaly
90.8216°
Eccentric anomaly
90.84021°
Mean motion
3.74749 °/min
Orbital period
96.06 mins
BSTAR
0.000052935
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Other satellites on launch #37 in the year 2023 (2023-03-17 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-5862 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-16 20:26:06.818Z | 350.027° N | 2025-12-16 20:30:06.818Z | 65.679° ENE | 33.219° | 2025-12-16 20:33:06.818Z | 127.365° SE |
| 5 mins | 2025-12-17 10:28:06.818Z | 149.047° SSE | 2025-12-17 10:30:06.818Z | 104.809° ESE | 25.434° | 2025-12-17 10:33:06.818Z | 51.365° ENE |
| 5 mins | 2025-12-17 12:06:06.818Z | 261.145° W | 2025-12-17 12:08:06.818Z | 298.637° NW | 22.075° | 2025-12-17 12:11:06.818Z | 352.511° N |
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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