STARLINK-32147, 60152
Orbit data source: Space-Track
STARLINK-32147, 60152 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 27 Jun 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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60152 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-32147
1 60152U 24120T 26171.36329560 -.00003762 00000-0 -10031-3 0 9992
2 60152 53.1588 202.4717 0001365 75.9951 284.1203 15.34385366112109Epoch: 2026-06-20T08:43Z
TLE epoch observation values (Epoch: 2026-06-20T08:43:08.739Z)
Latitude
-0.00006°
Longitude
163.10625°
Altitude
463.42 km
Speed
7.636 km/s
True Right ascension
13h 29m 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
07:12:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.938 km
Perigee altitude
462.07 km
Semi-major axis
6,841.141 km
Eccentricity
0.00014
Inclination
53.1588°
RAAN
202.4717°
Arg. of periapsis
75.9951°
True anomaly
284.10513°
Mean anomaly
284.1203°
Eccentric anomaly
284.11272°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
-0.00010031
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Other satellites on launch #120 in the year 2024 (2024-06-27 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-32147 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 05:15:31.738Z | 257.254° W | 2026-06-21 05:17:31.738Z | 336.201° NNW | 37.983° | 2026-06-21 05:20:31.738Z | 40.462° NE |
| 4 mins | 2026-06-21 10:11:31.738Z | 346.236° N | 2026-06-21 10:13:31.738Z | 29.734° NE | 19.853° | 2026-06-21 10:15:31.738Z | 69.54° E |
| 5 mins | 2026-06-21 11:49:31.738Z | 296.127° NW | 2026-06-21 11:51:31.738Z | 195.645° SSW | 41.019° | 2026-06-21 11:54:31.738Z | 142.487° SSE |
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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