STARLINK-4726, 53802
Orbit data source: Space-Track
STARLINK-4726, 53802 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 11 Sep 2022 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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53802 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-4726
1 53802U 22111AF 25258.18906310 .00001820 00000-0 13238-3 0 9996
2 53802 53.2178 331.8446 0001131 88.7434 271.3688 15.08842028167327Epoch: 2025-09-15T04:32Z
TLE epoch observation values (Epoch: 2025-09-15T04:32:15.051Z)
Latitude
-0.00002°
Longitude
-90.61542°
Altitude
540.616 km
Speed
7.593 km/s
True Right ascension
22h 07m 22s
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
08:27:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.765 km
Perigee altitude
539.2 km
Semi-major axis
6,918.119 km
Eccentricity
0.00011
Inclination
53.2178°
RAAN
331.8446°
Arg. of periapsis
88.7434°
True anomaly
271.35584°
Mean anomaly
271.3688°
Eccentric anomaly
271.36232°
Mean motion
3.77191 °/min
Orbital period
95.44 mins
BSTAR
0.00013238
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Other satellites on launch #111 in the year 2022 (2022-09-11 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-4726 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 | 2025-09-16 07:45:14.864Z | 235.542° WSW | 2025-09-16 07:48:14.864Z | 332.99° NNW | 44.273° | 2025-09-16 07:51:14.864Z | 46.231° ENE |
| 4 mins | 2025-09-16 09:26:14.864Z | 306.584° NW | 2025-09-16 09:28:14.864Z | 343.34° N | 18.108° | 2025-09-16 09:30:14.864Z | 17.762° NNE |
| 5 mins | 2025-09-16 12:47:14.864Z | 343.815° N | 2025-09-16 12:49:14.864Z | 21.256° NNE | 20.117° | 2025-09-16 12:52:14.864Z | 72.086° E |
| 6 mins | 2025-09-16 14:26:14.864Z | 308.063° NW | 2025-09-16 14:29:14.864Z | 170.144° S | 44.529° | 2025-09-16 14:32:14.864Z | 134.349° 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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