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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32265
1 60415U 24141T 25260.17777152 -.00002596 00000-0 -75602-4 0 9998
2 60415 53.1612 328.6400 0001259 110.0883 250.0253 15.30173373 63017Epoch: 2025-09-17T04:15Z
TLE epoch observation values (Epoch: 2025-09-17T04:15:59.459Z)
Latitude
-0.00004°
Longitude
-91.71523°
Altitude
476.489 km
Speed
7.629 km/s
True Right ascension
21h 54m 33s
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
19:12:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.414 km
Perigee altitude
474.688 km
Semi-major axis
6,853.688 km
Eccentricity
0.00013
Inclination
53.1612°
RAAN
328.64°
Arg. of periapsis
110.0883°
True anomaly
250.01174°
Mean anomaly
250.0253°
Eccentric anomaly
250.01852°
Mean motion
3.82522 °/min
Orbital period
94.11 mins
BSTAR
-0.000075602
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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 | 2025-09-18 07:05:10.497Z | 220.956° SW | 2025-09-18 07:08:10.497Z | 169.174° S | 42.958° | 2025-09-18 07:11:10.497Z | 55.398° ENE |
| 4 mins | 2025-09-18 08:45:10.497Z | 304.106° NW | 2025-09-18 08:46:10.497Z | 324.876° NNW | 18.999° | 2025-09-18 08:49:10.497Z | 23.095° NE |
| 5 mins | 2025-09-18 13:41:10.497Z | 322.086° NNW | 2025-09-18 13:43:10.497Z | 13.701° NNE | 40.067° | 2025-09-18 13:46:10.497Z | 114.765° 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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