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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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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-4600
1 53628U 22104AS 26259.25054243 .00000096 00000-0 13656-4 0 9992
2 53628 53.1578 87.4739 0001479 92.1194 267.9978 15.35395727224676Epoch: 2026-09-16T06:00Z
TLE epoch observation values (Epoch: 2026-09-16T06:00:46.865Z)
Latitude
-0.00008°
Longitude
2.07375°
Altitude
460.682 km
Speed
7.638 km/s
True Right ascension
05h 49m 53s
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
08:45:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.014 km
Perigee altitude
458.991 km
Semi-major axis
6,838.14 km
Eccentricity
0.00015
Inclination
53.1578°
RAAN
87.4739°
Arg. of periapsis
92.1194°
True anomaly
267.98086°
Mean anomaly
267.9978°
Eccentric anomaly
267.98933°
Mean motion
3.83828 °/min
Orbital period
93.79 mins
BSTAR
0.000013656
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-16 17:12:39.613Z | 294.988° NW | 2026-09-16 17:14:39.613Z | 328.922° NNW | 17.177° | 2026-09-16 17:16:39.613Z | 9.17° NNE |
| 5 mins | 2026-09-16 22:08:39.613Z | 316.632° NNW | 2026-09-16 22:10:39.613Z | 17.468° NNE | 73.069° | 2026-09-16 22:13:39.613Z | 123.715° SE |
| 5 mins | 2026-09-17 15:00:39.613Z | 217.953° SW | 2026-09-17 15:02:39.613Z | 131.151° SE | 72.381° | 2026-09-17 15:05:39.613Z | 54.356° ENE |
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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