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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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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32428
1 61666U 24193F 25290.48604024 .00000283 00000-0 21695-4 0 9990
2 61666 53.1619 36.0225 0001089 83.8885 276.2240 15.30191834 54601Epoch: 2025-10-17T11:39Z
TLE epoch observation values (Epoch: 2025-10-17T11:39:53.876Z)
Latitude
-0.00002°
Longitude
-165.18272°
Altitude
476.059 km
Speed
7.629 km/s
True Right ascension
02h 24m 05s
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
17:10:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.242 km
Perigee altitude
474.749 km
Semi-major axis
6,853.633 km
Eccentricity
0.00011
Inclination
53.1619°
RAAN
36.0225°
Arg. of periapsis
83.8885°
True anomaly
276.21159°
Mean anomaly
276.224°
Eccentric anomaly
276.2178°
Mean motion
3.82527 °/min
Orbital period
94.11 mins
BSTAR
0.000021695
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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 | 2025-10-18 09:47:15.388Z | 226.552° WSW | 2025-10-18 09:50:15.388Z | 192.694° SSW | 44.611° | 2025-10-18 09:53:15.388Z | 51.504° ENE |
| 4 mins | 2025-10-18 11:27:15.388Z | 307.192° NW | 2025-10-18 11:28:15.388Z | 327.055° NNW | 17.678° | 2025-10-18 11:31:15.388Z | 22.864° NE |
| 5 mins | 2025-10-18 16:23:15.388Z | 318.145° NNW | 2025-10-18 16:25:15.388Z | 10.702° NNE | 42.712° | 2025-10-18 16:28:15.388Z | 120.929° 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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