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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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: 1 day ago
TLE from 1 day ago
0 STARLINK-32122
1 60285U 24132H 25346.58346266 .00000644 00000-0 33909-4 0 9995
2 60285 53.1613 97.0626 0001299 83.8923 276.2226 15.30172389 78221Epoch: 2025-12-12T14:00Z
TLE epoch observation values (Epoch: 2025-12-12T14:00:11.173Z)
Latitude
-0.00002°
Longitude
165.49303°
Altitude
476.101 km
Speed
7.629 km/s
True Right ascension
06h 28m 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
16:29:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.444 km
Perigee altitude
474.663 km
Semi-major axis
6,853.691 km
Eccentricity
0.00013
Inclination
53.1613°
RAAN
97.0626°
Arg. of periapsis
83.8923°
True anomaly
276.2078°
Mean anomaly
276.2226°
Eccentric anomaly
276.2152°
Mean motion
3.82522 °/min
Orbital period
94.11 mins
BSTAR
0.000033909
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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 | 2025-12-14 10:05:33.823Z | 239.798° WSW | 2025-12-14 10:07:33.823Z | 269.566° W | 40.813° | 2025-12-14 10:11:33.823Z | 45.974° ENE |
| 4 mins | 2025-12-14 15:02:33.823Z | 340.877° N | 2025-12-14 15:04:33.823Z | 17.238° NNE | 17.852° | 2025-12-14 15:06:33.823Z | 57.661° ENE |
| 6 mins | 2025-12-14 16:40:33.823Z | 308.485° NW | 2025-12-14 16:43:33.823Z | 143.122° SSE | 42.639° | 2025-12-14 16:46:33.823Z | 133.089° 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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