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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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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-5692
1 55483U 23015AL 26083.48506435 .00009098 00000-0 34891-3 0 9994
2 55483 43.0008 255.6940 0001244 247.8593 112.2126 15.26693591172868Epoch: 2026-03-24T11:38Z
TLE epoch observation values (Epoch: 2026-03-24T11:38:29.559Z)
Latitude
-0.00006°
Longitude
-100.89127°
Altitude
485.803 km
Speed
7.624 km/s
True Right ascension
17h 02m 46s
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
05:48:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.503 km
Perigee altitude
486.795 km
Semi-major axis
6,865.786 km
Eccentricity
0.00012
Inclination
43.0008°
RAAN
255.694°
Arg. of periapsis
247.8593°
True anomaly
112.2258°
Mean anomaly
112.2126°
Eccentric anomaly
112.2192°
Mean motion
3.81512 °/min
Orbital period
94.36 mins
BSTAR
0.00034891
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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 | 2026-03-25 14:32:45.199Z | 214.863° SW | 2026-03-25 14:35:45.199Z | 136.753° SSE | 31.652° | 2026-03-25 14:38:45.199Z | 82.566° E |
| 6 mins | 2026-03-25 16:11:45.199Z | 267.839° W | 2026-03-25 16:14:45.199Z | 27.81° NE | 40.828° | 2026-03-25 16:17:45.199Z | 70.162° E |
| 5 mins | 2026-03-25 17:51:45.199Z | 298.276° NW | 2026-03-25 17:53:45.199Z | 15.899° NNE | 38.892° | 2026-03-25 17:56:45.199Z | 82.3° E |
| 5 mins | 2026-03-25 19:30:45.199Z | 279.183° WNW | 2026-03-25 19:32:45.199Z | 198.14° SSW | 42.556° | 2026-03-25 19:35:45.199Z | 122.263° SE |
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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