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: 20 hours ago
TLE from 20 hours ago
0 STARLINK-32412
1 61680U 24193V 26305.08593262 .00018981 00000-0 62128-3 0 9990
2 61680 53.1608 71.2886 0001147 66.7206 293.3916 15.31729839112744Epoch: 2026-11-01T02:03Z
TLE epoch observation values (Epoch: 2026-11-01T02:03:44.578Z)
Latitude
-0.00002°
Longitude
-0.02952°
Altitude
471.24 km
Speed
7.632 km/s
True Right ascension
04h 45m 09s
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
18:03:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.693 km
Perigee altitude
470.122 km
Semi-major axis
6,849.045 km
Eccentricity
0.00011
Inclination
53.1608°
RAAN
71.2886°
Arg. of periapsis
66.7206°
True anomaly
293.37954°
Mean anomaly
293.3916°
Eccentric anomaly
293.38557°
Mean motion
3.82911 °/min
Orbital period
94.02 mins
BSTAR
0.00062128
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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 | 2026-11-02 11:09:00.924Z | 233.434° WSW | 2026-11-02 11:11:00.924Z | 20.312° NNE | 77.514° | 2026-11-02 11:14:00.924Z | 48.45° ENE |
| 4 mins | 2026-11-02 16:05:00.924Z | 342.127° N | 2026-11-02 16:07:00.924Z | 17.447° NNE | 17.06° | 2026-11-02 16:09:00.924Z | 55.077° ENE |
| 6 mins | 2026-11-02 17:43:00.924Z | 314.26° NW | 2026-11-02 17:45:00.924Z | 335.424° NNW | 64.13° | 2026-11-02 17:49:00.924Z | 126.372° 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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