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 spacecraft
Bus & Motor
STARLINK, Unknown motor
Mass
305 kg wet, ~290 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 10.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-5692
1 55483U 23015AL 25297.47650047 .00001132 00000-0 98938-4 0 9992
2 55483 43.0099 359.1543 0002436 281.7312 78.3257 15.02529108150114Epoch: 2025-10-24T11:26Z
TLE epoch observation values (Epoch: 2025-10-24T11:26:09.640Z)
Latitude
-0.00003°
Longitude
154.49325°
Altitude
558.538 km
Speed
7.584 km/s
True Right ascension
23h 56m 37s
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
19:39:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.713 km
Perigee altitude
559.333 km
Semi-major axis
6,939.16 km
Eccentricity
0.00024
Inclination
43.0099°
RAAN
359.1543°
Arg. of periapsis
281.7312°
True anomaly
78.35304°
Mean anomaly
78.3257°
Eccentric anomaly
78.33937°
Mean motion
3.75477 °/min
Orbital period
95.88 mins
BSTAR
0.000098938
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-25 06:46:04.783Z | 188.541° SSW | 2025-10-25 06:48:04.783Z | 154.905° SSE | 20.948° | 2025-10-25 06:51:04.783Z | 99.619° ESE |
| 6 mins | 2025-10-25 08:26:04.783Z | 247.26° WSW | 2025-10-25 08:29:04.783Z | 100.189° ESE | 44.517° | 2025-10-25 08:32:04.783Z | 72.766° E |
| 6 mins | 2025-10-25 10:07:04.783Z | 285.767° WNW | 2025-10-25 10:10:04.783Z | 19.797° NNE | 38.737° | 2025-10-25 10:13:04.783Z | 74.219° E |
| 6 mins | 2025-10-25 11:48:04.783Z | 290.6° WNW | 2025-10-25 11:51:04.783Z | 79.81° E | 43.138° | 2025-10-25 11:54:04.783Z | 103.354° ESE |
| 5 mins | 2025-10-25 13:29:04.783Z | 258.592° W | 2025-10-25 13:31:04.783Z | 213.336° SW | 27.157° | 2025-10-25 13:34:04.783Z | 155.951° 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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