STARLINK-5692, 55483
Orbit data source: Space-Track
STARLINK-5692, 55483 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 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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55483 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, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-5692
1 55483U 23015AL 25255.19657382 .00000005 00000-0 15434-4 0 9992
2 55483 43.0040 228.8936 0001367 272.4041 87.6644 15.02537761143755Epoch: 2025-09-12T04:43Z
TLE epoch observation values (Epoch: 2025-09-12T04:43:03.978Z)
Latitude
-0.00006°
Longitude
166.67921°
Altitude
558.814 km
Speed
7.584 km/s
True Right ascension
15h 15m 34s
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
23:46:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.946 km
Perigee altitude
560.049 km
Semi-major axis
6,939.134 km
Eccentricity
0.00014
Inclination
43.004°
RAAN
228.8936°
Arg. of periapsis
272.4041°
True anomaly
87.68005°
Mean anomaly
87.6644°
Eccentric anomaly
87.67223°
Mean motion
3.75479 °/min
Orbital period
95.88 mins
BSTAR
0.000015434
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Other satellites on launch #15 in the year 2023 (2023-02-02 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-5692 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 | 2025-09-14 01:37:14.342Z | 232.905° WSW | 2025-09-14 01:40:14.342Z | 163.968° S | 41.413° | 2025-09-14 01:44:14.342Z | 75.666° E |
| 6 mins | 2025-09-14 03:18:14.342Z | 277.288° WNW | 2025-09-14 03:21:14.342Z | 4.715° NNE | 40.49° | 2025-09-14 03:24:14.342Z | 70.138° E |
| 6 mins | 2025-09-14 04:59:14.342Z | 292.087° WNW | 2025-09-14 05:02:14.342Z | 30.643° NE | 42.196° | 2025-09-14 05:05:14.342Z | 92.029° ESE |
| 6 mins | 2025-09-14 06:40:14.342Z | 271.462° WNW | 2025-09-14 06:42:14.342Z | 227.393° WSW | 34.659° | 2025-09-14 06:46:14.342Z | 137.356° SSE |
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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