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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 STARLINK-5692
1 55483U 23015AL 25302.39585086 -.00004630 00000-0 -32781-3 0 9991
2 55483 43.0057 332.4245 0001617 276.4873 83.5785 15.02547019150850Epoch: 2025-10-29T09:30Z
TLE epoch observation values (Epoch: 2025-10-29T09:30:01.514Z)
Latitude
-0.00003°
Longitude
151.94856°
Altitude
558.699 km
Speed
7.584 km/s
True Right ascension
22h 09m 41s
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
18:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.091 km
Perigee altitude
559.847 km
Semi-major axis
6,939.106 km
Eccentricity
0.00016
Inclination
43.0057°
RAAN
332.4245°
Arg. of periapsis
276.4873°
True anomaly
83.59691°
Mean anomaly
83.5785°
Eccentric anomaly
83.58771°
Mean motion
3.75481 °/min
Orbital period
95.88 mins
BSTAR
-0.00032781
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-30 04:50:13.847Z | 195.381° SSW | 2025-10-30 04:53:13.847Z | 136.403° SSE | 23.898° | 2025-10-30 04:56:13.847Z | 89.465° E |
| 7 mins | 2025-10-30 06:30:13.847Z | 252.509° W | 2025-10-30 06:33:13.847Z | 330.77° NNW | 44.971° | 2025-10-30 06:37:13.847Z | 71.803° E |
| 7 mins | 2025-10-30 08:11:13.847Z | 286.29° WNW | 2025-10-30 08:14:13.847Z | 6.352° NNE | 39.309° | 2025-10-30 08:18:13.847Z | 78.832° E |
| 6 mins | 2025-10-30 09:52:13.847Z | 288.708° WNW | 2025-10-30 09:55:13.847Z | 94.23° ESE | 44.611° | 2025-10-30 09:58:13.847Z | 107.743° ESE |
| 5 mins | 2025-10-30 11:33:13.847Z | 258.182° W | 2025-10-30 11:35:13.847Z | 218.654° SW | 24.043° | 2025-10-30 11:38:13.847Z | 162.739° S |
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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