STARLINK-32474, 61260
Orbit data source: Space-Track
STARLINK-32474, 61260 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 25 Sep 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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61260 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-32474
1 61260U 24175T 25304.75241067 -.00000144 00000-0 72664-5 0 9990
2 61260 53.1611 72.8724 0001497 96.5215 263.5956 15.30164272 61715Epoch: 2025-10-31T18:03Z
TLE epoch observation values (Epoch: 2025-10-31T18:03:28.281Z)
Latitude
-0.00006°
Longitude
121.71218°
Altitude
476.336 km
Speed
7.629 km/s
True Right ascension
04h 51m 29s
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
02:05:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.604 km
Perigee altitude
474.552 km
Semi-major axis
6,853.715 km
Eccentricity
0.00015
Inclination
53.1611°
RAAN
72.8724°
Arg. of periapsis
96.5215°
True anomaly
263.57855°
Mean anomaly
263.5956°
Eccentric anomaly
263.58708°
Mean motion
3.8252 °/min
Orbital period
94.11 mins
BSTAR
0.0000072664
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Other satellites on launch #175 in the year 2024 (2024-09-25 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-32474 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 | 2025-11-01 11:30:23.773Z | 232.865° WSW | 2025-11-01 11:32:23.773Z | 34.231° NE | 43.604° | 2025-11-01 11:35:23.773Z | 48.943° ENE |
| 4 mins | 2025-11-01 16:26:23.773Z | 339.615° N | 2025-11-01 16:28:23.773Z | 13.676° NNE | 16.342° | 2025-11-01 16:30:23.773Z | 52.582° ENE |
| 5 mins | 2025-11-01 18:05:23.773Z | 315.764° NNW | 2025-11-01 18:07:23.773Z | 91.097° ESE | 43.743° | 2025-11-01 18:10:23.773Z | 126.495° 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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