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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-32412
1 61680U 24193V 26127.25003472 -.00012863 00000-0 -40315-3 0 9999
2 61680 53.1594 179.2222 0001214 83.6251 118.9554 15.31721954 5813Epoch: 2026-05-07T06:00Z
TLE epoch observation values (Epoch: 2026-05-07T06:00:02.999Z)
Latitude
-18.08095°
Longitude
58.18918°
Altitude
476.025 km
Speed
7.628 km/s
True Right ascension
00h 53m 12s
True Declination
-17° 58' 32"
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
20:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.763 km
Perigee altitude
470.1 km
Semi-major axis
6,849.068 km
Eccentricity
0.00012
Inclination
53.1594°
RAAN
179.2222°
Arg. of periapsis
83.6251°
True anomaly
118.96757°
Mean anomaly
118.9554°
Eccentric anomaly
118.96149°
Mean motion
3.82909 °/min
Orbital period
94.02 mins
BSTAR
-0.00040315
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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 | 2026-05-07 13:27:42.051Z | 302.697° NW | 2026-05-07 13:30:42.051Z | 216.055° SW | 41.869° | 2026-05-07 13:33:42.051Z | 143.018° SSE |
| 5 mins | 2026-05-08 06:22:42.051Z | 244.018° WSW | 2026-05-08 06:24:42.051Z | 286.949° WNW | 40.658° | 2026-05-08 06:27:42.051Z | 41.758° NE |
| 4 mins | 2026-05-08 11:19:42.051Z | 346.419° N | 2026-05-08 11:21:42.051Z | 27.176° NE | 18.428° | 2026-05-08 11:23:42.051Z | 65.17° ENE |
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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