STARLINK-32404, 61710
Orbit data source: Space-Track
STARLINK-32404, 61710 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 30 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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61710 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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-32404
1 61710U 24196D 25260.21373044 -.00003399 00000-0 -10266-3 0 9990
2 61710 53.1608 187.3312 0001333 81.1027 279.0124 15.30202447 50596Epoch: 2025-09-17T05:07Z
TLE epoch observation values (Epoch: 2025-09-17T05:07:46.31Z)
Latitude
-0.00005°
Longitude
113.99531°
Altitude
475.965 km
Speed
7.629 km/s
True Right ascension
12h 29m 19s
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
16:38:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.378 km
Perigee altitude
474.55 km
Semi-major axis
6,853.601 km
Eccentricity
0.00013
Inclination
53.1608°
RAAN
187.3312°
Arg. of periapsis
81.1027°
True anomaly
278.99731°
Mean anomaly
279.0124°
Eccentric anomaly
279.00486°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
-0.00010266
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Other satellites on launch #196 in the year 2024 (2024-10-30 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-32404 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 03:32:49.752Z | 347.653° N | 2025-09-18 03:34:49.752Z | 35.903° NE | 22.351° | 2025-09-18 03:36:49.752Z | 76.094° E |
| 5 mins | 2025-09-18 05:10:49.752Z | 288.268° WNW | 2025-09-18 05:12:49.752Z | 209.978° SW | 37.136° | 2025-09-18 05:15:49.752Z | 150.114° SSE |
| 5 mins | 2025-09-18 22:05:49.752Z | 254.181° W | 2025-09-18 22:07:49.752Z | 305.691° NW | 37.226° | 2025-09-18 22:10:49.752Z | 37.36° NE |
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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