STARLINK-32122, 60285
Orbit data source: Space-Track
STARLINK-32122, 60285 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 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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60285 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32122
1 60285U 24132H 26062.05125125 -.00000295 00000-0 21699-5 0 9999
2 60285 53.1608 83.2919 0001377 98.5263 261.5893 15.30188127 90547Epoch: 2026-03-03T01:13Z
TLE epoch observation values (Epoch: 2026-03-03T01:13:48.107Z)
Latitude
-0.00012°
Longitude
-95.9945°
Altitude
476.288 km
Speed
7.629 km/s
True Right ascension
05h 33m 10s
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
15:42:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.451 km
Perigee altitude
474.563 km
Semi-major axis
6,853.644 km
Eccentricity
0.00014
Inclination
53.1608°
RAAN
83.2919°
Arg. of periapsis
98.5263°
True anomaly
261.57369°
Mean anomaly
261.5893°
Eccentric anomaly
261.5815°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
0.0000021699
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Other satellites on launch #132 in the year 2024 (2024-07-28 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-32122 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 | 2026-03-04 04:04:17.227Z | 235.187° WSW | 2026-03-04 04:07:17.227Z | 22.918° NE | 42.347° | 2026-03-04 04:10:17.227Z | 47.54° ENE |
| 4 mins | 2026-03-04 09:01:17.227Z | 340.431° N | 2026-03-04 09:03:17.227Z | 15.628° NNE | 17.01° | 2026-03-04 09:05:17.227Z | 55.098° ENE |
| 6 mins | 2026-03-04 10:39:17.227Z | 311.223° NW | 2026-03-04 10:42:17.227Z | 119.18° SE | 43.434° | 2026-03-04 10:45:17.227Z | 129.523° 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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