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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-32474
1 61260U 24175T 25290.97096291 -.00004029 00000-0 -12388-3 0 9997
2 61260 53.1590 136.8851 0001190 95.9529 264.1608 15.30221447 59608Epoch: 2025-10-17T23:18Z
TLE epoch observation values (Epoch: 2025-10-17T23:18:11.195Z)
Latitude
0.00003°
Longitude
120.62979°
Altitude
476.134 km
Speed
7.629 km/s
True Right ascension
09h 07m 32s
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
23:58:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.223 km
Perigee altitude
474.592 km
Semi-major axis
6,853.545 km
Eccentricity
0.00012
Inclination
53.159°
RAAN
136.8851°
Arg. of periapsis
95.9529°
True anomaly
264.14723°
Mean anomaly
264.1608°
Eccentric anomaly
264.15402°
Mean motion
3.82534 °/min
Orbital period
94.11 mins
BSTAR
-0.00012388
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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 | 2025-10-18 16:44:58.218Z | 237.262° WSW | 2025-10-18 16:46:58.218Z | 333.609° NNW | 44.292° | 2025-10-18 16:49:58.218Z | 46.87° ENE |
| 5 mins | 2025-10-18 23:19:58.218Z | 311.548° NW | 2025-10-18 23:21:58.218Z | 31.736° NE | 44.957° | 2025-10-18 23:24:58.218Z | 129.593° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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