STARLINK-32020, 60201
Orbit data source: Space-Track
STARLINK-32020, 60201 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 03 Jul 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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60201 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 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-32020
1 60201U 24124U 25308.64105961 -.00000259 00000-0 34064-5 0 9991
2 60201 53.1575 183.0829 0001618 94.8619 265.2567 15.30200367 75159Epoch: 2025-11-04T15:23Z
TLE epoch observation values (Epoch: 2025-11-04T15:23:07.550Z)
Latitude
0.00003°
Longitude
-91.82371°
Altitude
476.205 km
Speed
7.629 km/s
True Right ascension
12h 12m 19s
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
02:41:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.58 km
Perigee altitude
474.362 km
Semi-major axis
6,853.608 km
Eccentricity
0.00016
Inclination
53.1575°
RAAN
183.0829°
Arg. of periapsis
94.8619°
True anomaly
265.23822°
Mean anomaly
265.2567°
Eccentric anomaly
265.24746°
Mean motion
3.82529 °/min
Orbital period
94.11 mins
BSTAR
0.0000034064
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Other satellites on launch #124 in the year 2024 (2024-07-03 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-32020 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 | 2025-11-05 18:11:55.458Z | 221.84° SW | 2025-11-05 18:15:55.458Z | 87.636° E | 41.766° | 2025-11-05 18:18:55.458Z | 54.001° ENE |
| 4 mins | 2025-11-05 23:09:55.458Z | 342.144° N | 2025-11-05 23:11:55.458Z | 16.146° NNE | 14.762° | 2025-11-05 23:13:55.458Z | 51.395° ENE |
| 5 mins | 2025-11-06 00:48:55.458Z | 327.504° NNW | 2025-11-06 00:50:55.458Z | 68.305° E | 39.648° | 2025-11-06 00:53:55.458Z | 117.584° 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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