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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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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-32002
1 60200U 24124T 25260.72744684 -.00000063 00000-0 10013-4 0 9997
2 60200 53.1620 45.9397 0001177 92.9300 267.1835 15.30195310 67815Epoch: 2025-09-17T17:27Z
TLE epoch observation values (Epoch: 2025-09-17T17:27:31.406Z)
Latitude
-0.00009°
Longitude
147.15953°
Altitude
476.169 km
Speed
7.629 km/s
True Right ascension
03h 03m 45s
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
21:04:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.292 km
Perigee altitude
474.679 km
Semi-major axis
6,853.622 km
Eccentricity
0.00012
Inclination
53.162°
RAAN
45.9397°
Arg. of periapsis
92.93°
True anomaly
267.17003°
Mean anomaly
267.1835°
Eccentric anomaly
267.17676°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000010013
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-19 11:57:05.326Z | 220.942° SW | 2025-09-19 12:00:05.326Z | 179.534° S | 42.231° | 2025-09-19 12:03:05.326Z | 55.836° ENE |
| 4 mins | 2025-09-19 13:37:05.326Z | 302.135° NW | 2025-09-19 13:39:05.326Z | 346.129° N | 19.061° | 2025-09-19 13:41:05.326Z | 21.854° NNE |
| 5 mins | 2025-09-19 18:33:05.326Z | 321.586° NNW | 2025-09-19 18:35:05.326Z | 6.637° NNE | 39.38° | 2025-09-19 18:38:05.326Z | 114.015° 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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