STARLINK-32428, 61666
Orbit data source: Space-Track
STARLINK-32428, 61666 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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61666 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-32428
1 61666U 24193F 26125.54519413 -.00000033 00000-0 10994-4 0 9996
2 61666 53.1589 186.7633 0000963 84.7989 275.3122 15.30196550 85230Epoch: 2026-05-05T13:05Z
TLE epoch observation values (Epoch: 2026-05-05T13:05:04.772Z)
Latitude
-0.00001°
Longitude
127.07491°
Altitude
476.064 km
Speed
7.629 km/s
True Right ascension
12h 27m 03s
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
05:25:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.142 km
Perigee altitude
474.822 km
Semi-major axis
6,853.619 km
Eccentricity
0.0001
Inclination
53.1589°
RAAN
186.7633°
Arg. of periapsis
84.7989°
True anomaly
275.30121°
Mean anomaly
275.3122°
Eccentric anomaly
275.30671°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000010994
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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-32428 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 | 2026-05-06 06:30:12.890Z | 211.949° SW | 2026-05-06 06:33:12.890Z | 105.171° ESE | 39.023° | 2026-05-06 06:36:12.890Z | 57.576° ENE |
| 4 mins | 2026-05-06 08:09:12.890Z | 295.159° NW | 2026-05-06 08:11:12.890Z | 340.445° N | 21.008° | 2026-05-06 08:13:12.890Z | 20.044° NNE |
| 5 mins | 2026-05-06 13:06:12.890Z | 334° NNW | 2026-05-06 13:08:12.890Z | 59.179° ENE | 36.351° | 2026-05-06 13:11:12.890Z | 111.735° ESE |
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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