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 25337.14852869 -.00000526 00000-0 -56461-5 0 9999
2 61260 53.1625 282.3967 0001221 94.9892 265.1248 15.30186973 66679Epoch: 2025-12-03T03:33Z
TLE epoch observation values (Epoch: 2025-12-03T03:33:52.878Z)
Latitude
-0.00005°
Longitude
156.70285°
Altitude
476.225 km
Speed
7.629 km/s
True Right ascension
18h 49m 35s
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
13:20:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.347 km
Perigee altitude
474.673 km
Semi-major axis
6,853.647 km
Eccentricity
0.00012
Inclination
53.1625°
RAAN
282.3967°
Arg. of periapsis
94.9892°
True anomaly
265.11086°
Mean anomaly
265.1248°
Eccentric anomaly
265.11783°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.0000056461
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-03 22:31:34.745Z | 197.748° SSW | 2025-12-03 22:34:34.745Z | 142.636° SSE | 28.691° | 2025-12-03 22:37:34.745Z | 71.517° E |
| 5 mins | 2025-12-04 00:10:34.745Z | 275.861° WNW | 2025-12-04 00:12:34.745Z | 323.333° NNW | 27.315° | 2025-12-04 00:15:34.745Z | 30.027° NE |
| 5 mins | 2025-12-04 05:07:34.745Z | 337.109° NNW | 2025-12-04 05:09:34.745Z | 27.38° NE | 28.494° | 2025-12-04 05:12:34.745Z | 93.898° ESE |
| 5 mins | 2025-12-04 06:45:34.745Z | 278.312° WNW | 2025-12-04 06:47:34.745Z | 227.091° WSW | 27.369° | 2025-12-04 06:50:34.745Z | 166.39° S |
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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