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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32122
1 60285U 24132H 26303.41670139 -.00027273 00000-0 -82056-3 0 9995
2 60285 53.1605 40.8054 0001221 89.7896 35.5484 15.33562345 5840Epoch: 2026-10-30T10:00Z
TLE epoch observation values (Epoch: 2026-10-30T10:00:03.000Z)
Latitude
40.88465°
Longitude
-8.11066°
Altitude
468.291 km
Speed
7.638 km/s
True Right ascension
12h 02m 33s
True Declination
40° 42' 26"
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
15:44:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.286 km
Perigee altitude
464.615 km
Semi-major axis
6,843.588 km
Eccentricity
0.00012
Inclination
53.1605°
RAAN
40.8054°
Arg. of periapsis
89.7896°
True anomaly
35.55654°
Mean anomaly
35.5484°
Eccentric anomaly
35.55247°
Mean motion
3.83369 °/min
Orbital period
93.9 mins
BSTAR
-0.00082056
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-31 09:04:58.388Z | 219.986° SW | 2026-10-31 09:07:58.388Z | 186.466° SSW | 58.293° | 2026-10-31 09:11:58.388Z | 54.619° ENE |
| 4 mins | 2026-10-31 10:44:58.388Z | 302.644° NW | 2026-10-31 10:45:58.388Z | 323.506° NNW | 20.269° | 2026-10-31 10:48:58.388Z | 22.712° NE |
| 5 mins | 2026-10-31 15:40:58.388Z | 330.281° NNW | 2026-10-31 15:42:58.388Z | 60.546° ENE | 51.999° | 2026-10-31 15:45:58.388Z | 114.658° 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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