STARLINK-32113, 60282
Orbit data source: Space-Track
STARLINK-32113, 60282 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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60282 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-32113
1 60282U 24132E 25303.26602882 .00000107 00000-0 15734-4 0 9999
2 60282 53.1606 298.1148 0001504 83.5822 276.5350 15.30196832 71590Epoch: 2025-10-30T06:23Z
TLE epoch observation values (Epoch: 2025-10-30T06:23:04.890Z)
Latitude
0°
Longitude
163.51714°
Altitude
476.007 km
Speed
7.629 km/s
True Right ascension
19h 52m 27s
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
17:44:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.512 km
Perigee altitude
474.45 km
Semi-major axis
6,853.618 km
Eccentricity
0.00015
Inclination
53.1606°
RAAN
298.1148°
Arg. of periapsis
83.5822°
True anomaly
276.51788°
Mean anomaly
276.535°
Eccentric anomaly
276.52644°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000015734
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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-32113 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-31 01:20:33.668Z | 173.218° S | 2025-10-31 01:23:33.668Z | 118.617° SE | 17.243° | 2025-10-31 01:25:33.668Z | 84.847° E |
| 5 mins | 2025-10-31 02:58:33.668Z | 255.2° W | 2025-10-31 03:00:33.668Z | 312.386° NW | 37.56° | 2025-10-31 03:03:33.668Z | 37.972° NE |
| 4 mins | 2025-10-31 07:55:33.668Z | 342.962° N | 2025-10-31 07:57:33.668Z | 24.895° NE | 20.917° | 2025-10-31 07:59:33.668Z | 67.682° E |
| 5 mins | 2025-10-31 09:33:33.668Z | 297.52° NW | 2025-10-31 09:35:33.668Z | 240.737° WSW | 40.471° | 2025-10-31 09:38:33.668Z | 146.282° SSE |
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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