STARLINK-4693, 53605
Orbit data source: Space-Track
STARLINK-4693, 53605 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 Aug 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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53605 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
300 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-4693
1 53605U 22104T 25300.51829728 .00003866 00000-0 26087-3 0 9999
2 53605 53.2152 121.7253 0001477 96.9632 263.1528 15.08837626175516Epoch: 2025-10-27T12:26Z
TLE epoch observation values (Epoch: 2025-10-27T12:26:20.884Z)
Latitude
-0.00001°
Longitude
-100.98072°
Altitude
540.77 km
Speed
7.593 km/s
True Right ascension
08h 06m 54s
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
20:23:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.018 km
Perigee altitude
538.974 km
Semi-major axis
6,918.133 km
Eccentricity
0.00015
Inclination
53.2152°
RAAN
121.7253°
Arg. of periapsis
96.9632°
True anomaly
263.136°
Mean anomaly
263.1528°
Eccentric anomaly
263.1444°
Mean motion
3.7719 °/min
Orbital period
95.44 mins
BSTAR
0.00026087
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Other satellites on launch #104 in the year 2022 (2022-08-28 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-4693 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 | 2025-10-28 14:01:18.081Z | 194.925° SSW | 2025-10-28 14:04:18.081Z | 147.441° SSE | 27.682° | 2025-10-28 14:08:18.081Z | 68.214° E |
| 5 mins | 2025-10-28 15:42:18.081Z | 278.942° WNW | 2025-10-28 15:44:18.081Z | 336.341° NNW | 30.747° | 2025-10-28 15:47:18.081Z | 33.572° NE |
| 5 mins | 2025-10-28 20:43:18.081Z | 337.803° N | 2025-10-28 20:45:18.081Z | 27.121° NE | 30.283° | 2025-10-28 20:48:18.081Z | 93.01° ESE |
| 6 mins | 2025-10-28 22:22:18.081Z | 283.316° WNW | 2025-10-28 22:24:18.081Z | 242.172° WSW | 28.677° | 2025-10-28 22:28:18.081Z | 163.365° 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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