STARLINK-5892, 55954
Orbit data source: Space-Track
STARLINK-5892, 55954 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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55954 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: 20 hours ago
TLE from 20 hours ago
0 STARLINK-5892
1 55954U 23037AS 25348.76363175 .00001062 00000-0 96771-4 0 9996
2 55954 69.9994 118.5224 0003157 269.0617 91.0181 14.98329163151751Epoch: 2025-12-14T18:19Z
TLE epoch observation values (Epoch: 2025-12-14T18:19:37.783Z)
Latitude
0.00005°
Longitude
119.94311°
Altitude
574.522 km
Speed
7.574 km/s
True Right ascension
07h 54m 05s
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
13:19:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.2 km
Perigee altitude
567.813 km
Semi-major axis
6,948.144 km
Eccentricity
0.00032
Inclination
69.9994°
RAAN
118.5224°
Arg. of periapsis
269.0617°
True anomaly
91.05427°
Mean anomaly
91.0181°
Eccentric anomaly
91.03619°
Mean motion
3.74749 °/min
Orbital period
96.06 mins
BSTAR
0.000096771
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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-5892 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 | 2025-12-15 18:53:28.366Z | 3.569° NNE | 2025-12-15 18:56:28.366Z | 49.803° ENE | 20.923° | 2025-12-15 18:59:28.366Z | 103.121° ESE |
| 6 mins | 2025-12-15 20:32:28.366Z | 305.491° NW | 2025-12-15 20:35:28.366Z | 241.452° WSW | 26.451° | 2025-12-15 20:38:28.366Z | 193.03° SSW |
| 6 mins | 2025-12-16 10:32:28.366Z | 234.059° WSW | 2025-12-16 10:35:28.366Z | 315.089° NNW | 34.12° | 2025-12-16 10:38:28.366Z | 8.482° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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