STARLINK-32002, 60200
Orbit data source: Space-Track
STARLINK-32002, 60200 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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60200 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-32002
1 60200U 24124T 26305.72038776 -.00000148 00000-0 69859-5 0 9993
2 60200 53.1608 299.5652 0001361 83.1722 276.9434 15.31699483130610Epoch: 2026-11-01T17:17Z
TLE epoch observation values (Epoch: 2026-11-01T17:17:21.502Z)
Latitude
-0.00004°
Longitude
-0.78213°
Altitude
471.529 km
Speed
7.632 km/s
True Right ascension
19h 58m 15s
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
04:14:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.93 km
Perigee altitude
470.066 km
Semi-major axis
6,849.135 km
Eccentricity
0.00014
Inclination
53.1608°
RAAN
299.5652°
Arg. of periapsis
83.1722°
True anomaly
276.92792°
Mean anomaly
276.9434°
Eccentric anomaly
276.93566°
Mean motion
3.82904 °/min
Orbital period
94.02 mins
BSTAR
0.0000069859
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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-32002 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 | 2026-11-02 09:26:52.902Z | 308.126° NW | 2026-11-02 09:29:52.902Z | 286.918° WNW | 69.589° | 2026-11-02 09:33:52.902Z | 134.556° SE |
| 5 mins | 2026-11-03 02:22:52.902Z | 237.436° WSW | 2026-11-03 02:24:52.902Z | 10.203° NNE | 72.377° | 2026-11-03 02:27:52.902Z | 47.259° ENE |
| 4 mins | 2026-11-03 07:18:52.902Z | 342.243° N | 2026-11-03 07:20:52.902Z | 18.13° NNE | 17.605° | 2026-11-03 07:22:52.902Z | 56.378° 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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