STARLINK-32202, 60595
Orbit data source: Space-Track
STARLINK-32202, 60595 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 20 Aug 2024 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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60595 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32202
1 60595U 24150N 26171.31518308 .00000836 00000-0 38701-4 0 9993
2 60595 53.1596 190.3541 0000955 82.6216 277.4894 15.31704241103758Epoch: 2026-06-20T07:33Z
TLE epoch observation values (Epoch: 2026-06-20T07:33:51.818Z)
Latitude
0.00001°
Longitude
168.35662°
Altitude
471.542 km
Speed
7.632 km/s
True Right ascension
12h 41m 24s
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
07:13:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.638 km
Perigee altitude
470.33 km
Semi-major axis
6,849.121 km
Eccentricity
0.0001
Inclination
53.1596°
RAAN
190.3541°
Arg. of periapsis
82.6216°
True anomaly
277.47855°
Mean anomaly
277.4894°
Eccentric anomaly
277.48397°
Mean motion
3.82905 °/min
Orbital period
94.02 mins
BSTAR
0.000038701
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Other satellites on launch #150 in the year 2024 (2024-08-20 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-32202 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 04:07:25.870Z | 235.844° WSW | 2026-06-21 04:09:25.870Z | 314.369° NW | 44.492° | 2026-06-21 04:12:25.870Z | 47.216° ENE |
| 4 mins | 2026-06-21 09:03:25.870Z | 338.721° N | 2026-06-21 09:05:25.870Z | 12.6° NNE | 16.563° | 2026-06-21 09:07:25.870Z | 52.599° ENE |
| 5 mins | 2026-06-21 10:42:25.870Z | 313.293° NW | 2026-06-21 10:44:25.870Z | 111.348° ESE | 43.668° | 2026-06-21 10:47:25.870Z | 128.689° 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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