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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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-32404
1 61710U 24196D 26060.52543388 -.00000585 00000-0 -76508-5 0 9990
2 61710 53.1579 139.4765 0000822 85.2702 274.8393 15.30177321 75905Epoch: 2026-03-01T12:36Z
TLE epoch observation values (Epoch: 2026-03-01T12:36:37.487Z)
Latitude
0.00003°
Longitude
150.98838°
Altitude
476.135 km
Speed
7.629 km/s
True Right ascension
09h 17m 54s
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
03:42:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.103 km
Perigee altitude
474.976 km
Semi-major axis
6,853.677 km
Eccentricity
0.00008
Inclination
53.1579°
RAAN
139.4765°
Arg. of periapsis
85.2702°
True anomaly
274.82991°
Mean anomaly
274.8393°
Eccentric anomaly
274.83461°
Mean motion
3.82523 °/min
Orbital period
94.11 mins
BSTAR
-0.0000076508
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-02 07:35:11.203Z | 214.488° SW | 2026-03-02 07:38:11.203Z | 156.414° SSE | 39.831° | 2026-03-02 07:41:11.203Z | 59.997° ENE |
| 4 mins | 2026-03-02 09:15:11.203Z | 301.481° NW | 2026-03-02 09:16:11.203Z | 323.92° NNW | 20.855° | 2026-03-02 09:19:11.203Z | 24.454° NE |
| 5 mins | 2026-03-02 14:11:11.203Z | 326.563° NNW | 2026-03-02 14:13:11.203Z | 19.425° NNE | 36.908° | 2026-03-02 14:16:11.203Z | 108.274° 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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