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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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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32412
1 61680U 24193V 26306.65194882 .00016657 00000-0 54722-3 0 9998
2 61680 53.1607 63.9922 0001232 108.2351 251.8784 15.31706366112988Epoch: 2026-11-02T15:38Z
TLE epoch observation values (Epoch: 2026-11-02T15:38:48.378Z)
Latitude
-0.00005°
Longitude
147.36469°
Altitude
471.884 km
Speed
7.631 km/s
True Right ascension
04h 15m 58s
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
09:43:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.821 km
Perigee altitude
470.134 km
Semi-major axis
6,849.114 km
Eccentricity
0.00012
Inclination
53.1607°
RAAN
63.9922°
Arg. of periapsis
108.2351°
True anomaly
251.86498°
Mean anomaly
251.8784°
Eccentric anomaly
251.87169°
Mean motion
3.82905 °/min
Orbital period
94.02 mins
BSTAR
0.00054722
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 17:12:37.260Z | 321.576° NNW | 2026-11-03 17:14:37.260Z | 36.977° NE | 64.841° | 2026-11-03 17:17:37.260Z | 119.021° SE |
| 6 mins | 2026-11-04 10:06:37.260Z | 215.63° SW | 2026-11-04 10:08:37.260Z | 175.153° S | 60.777° | 2026-11-04 10:12:37.260Z | 54.877° ENE |
| 4 mins | 2026-11-04 11:45:37.260Z | 302.506° NW | 2026-11-04 11:46:37.260Z | 323.623° NNW | 20.825° | 2026-11-04 11:49:37.260Z | 22.974° NE |
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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