STARLINK-4600, 53628
Orbit data source: Space-Track
STARLINK-4600, 53628 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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53628 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: 2 days ago
TLE from 2 days ago
0 STARLINK-4600
1 53628U 22104AS 25299.90094670 .00000162 00000-0 28269-4 0 9995
2 53628 53.2162 114.2827 0001312 90.6252 269.4891 15.08840850175563Epoch: 2025-10-26T21:37Z
TLE epoch observation values (Epoch: 2025-10-26T21:37:21.794Z)
Latitude
-0°
Longitude
114.43139°
Altitude
540.646 km
Speed
7.593 km/s
True Right ascension
07h 37m 07s
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
07:09:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.894 km
Perigee altitude
539.078 km
Semi-major axis
6,918.123 km
Eccentricity
0.00013
Inclination
53.2162°
RAAN
114.2827°
Arg. of periapsis
90.6252°
True anomaly
269.47407°
Mean anomaly
269.4891°
Eccentric anomaly
269.48158°
Mean motion
3.77191 °/min
Orbital period
95.44 mins
BSTAR
0.000028269
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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-4600 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 13:31:14.545Z | 201.031° SSW | 2025-10-28 13:34:14.545Z | 149.122° SSE | 32.336° | 2025-10-28 13:38:14.545Z | 64.065° ENE |
| 5 mins | 2025-10-28 15:12:14.545Z | 285.409° WNW | 2025-10-28 15:14:14.545Z | 337.102° NNW | 27.725° | 2025-10-28 15:17:14.545Z | 31.782° NE |
| 5 mins | 2025-10-28 20:13:14.545Z | 334.668° NNW | 2025-10-28 20:15:14.545Z | 28.449° NE | 33.615° | 2025-10-28 20:18:14.545Z | 99.338° ESE |
| 5 mins | 2025-10-28 21:52:14.545Z | 277.774° WNW | 2025-10-28 21:54:14.545Z | 238.137° WSW | 24.75° | 2025-10-28 21:57:14.545Z | 177.269° 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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