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, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32412
1 61680U 24193V 25312.14323132 -.00001471 00000-0 -37554-4 0 9995
2 61680 53.1618 295.8345 0001281 63.4216 296.6916 15.30182573 57913Epoch: 2025-11-08T03:26Z
TLE epoch observation values (Epoch: 2025-11-08T03:26:15.186Z)
Latitude
0°
Longitude
-163.30585°
Altitude
475.773 km
Speed
7.629 km/s
True Right ascension
19h 43m 20s
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
09:27:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.401 km
Perigee altitude
474.645 km
Semi-major axis
6,853.66 km
Eccentricity
0.00013
Inclination
53.1618°
RAAN
295.8345°
Arg. of periapsis
63.4216°
True anomaly
296.67848°
Mean anomaly
296.6916°
Eccentric anomaly
296.68504°
Mean motion
3.82525 °/min
Orbital period
94.11 mins
BSTAR
-0.000037554
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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 | 2025-11-09 01:33:18.208Z | 220.688° SW | 2025-11-09 01:36:18.208Z | 162.456° S | 43.106° | 2025-11-09 01:39:18.208Z | 55.392° ENE |
| 4 mins | 2025-11-09 03:13:18.208Z | 304.973° NW | 2025-11-09 03:14:18.208Z | 326.067° NNW | 19.112° | 2025-11-09 03:17:18.208Z | 23.725° NE |
| 5 mins | 2025-11-09 08:09:18.208Z | 322.596° NNW | 2025-11-09 08:11:18.208Z | 18.198° NNE | 40.23° | 2025-11-09 08:14:18.208Z | 114.836° 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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