STARLINK-32412, 61680
Orbit data source: Space-Track
STARLINK-32412, 61680 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 26 Oct 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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61680 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-32412
1 61680U 24193V 25259.17294225 -.00000179 00000-0 60748-5 0 9993
2 61680 53.1595 181.8773 0000865 102.1758 257.9340 15.30182459 49808Epoch: 2025-09-16T04:09Z
TLE epoch observation values (Epoch: 2025-09-16T04:09:02.21Z)
Latitude
0.00001°
Longitude
124.25105°
Altitude
476.291 km
Speed
7.629 km/s
True Right ascension
12h 07m 30s
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
12:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.117 km
Perigee altitude
474.931 km
Semi-major axis
6,853.661 km
Eccentricity
0.00009
Inclination
53.1595°
RAAN
181.8773°
Arg. of periapsis
102.1758°
True anomaly
257.92431°
Mean anomaly
257.934°
Eccentric anomaly
257.92915°
Mean motion
3.82524 °/min
Orbital period
94.11 mins
BSTAR
0.0000060748
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Other satellites on launch #193 in the year 2024 (2024-10-26 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-32412 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 | 2025-09-16 21:34:27.021Z | 222.58° SW | 2025-09-16 21:37:27.021Z | 95.937° ESE | 43.602° | 2025-09-16 21:40:27.021Z | 53.175° ENE |
| 5 mins | 2025-09-17 04:10:27.021Z | 323.553° NNW | 2025-09-17 04:12:27.021Z | 55.691° ENE | 41.528° | 2025-09-17 04:15:27.021Z | 118.785° 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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