STARLINK-32265, 60415
Orbit data source: Space-Track
STARLINK-32265, 60415 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 10 Aug 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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60415 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32265
1 60415U 24141T 25343.58473950 -.00001421 00000-0 -35854-4 0 9995
2 60415 53.1607 301.2228 0001893 77.5571 282.5641 15.30179675 75780Epoch: 2025-12-09T14:02Z
TLE epoch observation values (Epoch: 2025-12-09T14:02:01.492Z)
Latitude
-0.00008°
Longitude
12.14921°
Altitude
475.894 km
Speed
7.629 km/s
True Right ascension
20h 04m 53s
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
22:04:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.829 km
Perigee altitude
474.235 km
Semi-major axis
6,853.669 km
Eccentricity
0.00019
Inclination
53.1607°
RAAN
301.2228°
Arg. of periapsis
77.5571°
True anomaly
282.54293°
Mean anomaly
282.5641°
Eccentric anomaly
282.55351°
Mean motion
3.82524 °/min
Orbital period
94.11 mins
BSTAR
-0.000035854
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Other satellites on launch #141 in the year 2024 (2024-08-10 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-32265 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 | 2025-12-10 01:13:36.899Z | 268.5° W | 2025-12-10 01:16:36.899Z | 324.137° NNW | 25.703° | 2025-12-10 01:19:36.899Z | 28.874° NE |
| 5 mins | 2025-12-10 06:11:36.899Z | 335.344° NNW | 2025-12-10 06:13:36.899Z | 27.371° NE | 30.259° | 2025-12-10 06:16:36.899Z | 96.932° ESE |
| 5 mins | 2025-12-10 07:49:36.899Z | 275.356° WNW | 2025-12-10 07:51:36.899Z | 226.801° WSW | 25.02° | 2025-12-10 07:54:36.899Z | 169.629° S |
| 5 mins | 2025-12-10 23:07:36.899Z | 180.764° SSW | 2025-12-10 23:09:36.899Z | 124.87° SE | 27.812° | 2025-12-10 23:12:36.899Z | 68.644° E |
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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