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: 2 days ago
TLE from 2 days ago
0 STARLINK-32412
1 61680U 24193V 26034.01186817 .00002152 00000-0 84799-4 0 9998
2 61680 53.1595 252.3351 0001357 91.3647 268.7510 15.30187672 71218Epoch: 2026-02-03T00:17Z
TLE epoch observation values (Epoch: 2026-02-03T00:17:05.409Z)
Latitude
0.00002°
Longitude
114.86366°
Altitude
476.172 km
Speed
7.629 km/s
True Right ascension
16h 49m 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
00:59:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.438 km
Perigee altitude
474.578 km
Semi-major axis
6,853.645 km
Eccentricity
0.00014
Inclination
53.1595°
RAAN
252.3351°
Arg. of periapsis
91.3647°
True anomaly
268.73545°
Mean anomaly
268.751°
Eccentric anomaly
268.74323°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
0.000084799
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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 | 2026-02-04 23:49:07.127Z | 303.803° NW | 2026-02-04 23:52:07.127Z | 245.563° WSW | 41.796° | 2026-02-04 23:55:07.127Z | 143.278° SSE |
| 5 mins | 2026-02-05 16:46:07.127Z | 249.307° W | 2026-02-05 16:48:07.127Z | 354.587° N | 40.862° | 2026-02-05 16:51:07.127Z | 44.068° NE |
| 4 mins | 2026-02-05 21:43:07.127Z | 352.779° N | 2026-02-05 21:44:07.127Z | 13.094° NNE | 18.364° | 2026-02-05 21:47:07.127Z | 70.256° E |
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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