STARLINK-32528, 61724
Orbit data source: Space-Track
STARLINK-32528, 61724 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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61724 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-32528
1 61724U 24196T 25306.40393920 .00001760 00000-0 71555-4 0 9999
2 61724 53.1612 332.9213 0001295 79.4606 280.6540 15.30190070 56464Epoch: 2025-11-02T09:41Z
TLE epoch observation values (Epoch: 2025-11-02T09:41:40.346Z)
Latitude
-0.00009°
Longitude
145.58297°
Altitude
475.981 km
Speed
7.629 km/s
True Right ascension
22h 11m 41s
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
17:40:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.389 km
Perigee altitude
474.613 km
Semi-major axis
6,853.638 km
Eccentricity
0.00013
Inclination
53.1612°
RAAN
332.9213°
Arg. of periapsis
79.4606°
True anomaly
280.63942°
Mean anomaly
280.654°
Eccentric anomaly
280.64671°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
0.000071555
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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-32528 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-04 04:11:22.351Z | 225.764° WSW | 2025-11-04 04:14:22.351Z | 210.122° SW | 42.505° | 2025-11-04 04:18:22.351Z | 51.672° ENE |
| 4 mins | 2025-11-04 09:09:22.351Z | 343.477° N | 2025-11-04 09:11:22.351Z | 18.785° NNE | 15.498° | 2025-11-04 09:13:22.351Z | 54.495° ENE |
| 6 mins | 2025-11-04 10:47:22.351Z | 317.577° NNW | 2025-11-04 10:50:22.351Z | 87.181° E | 40.336° | 2025-11-04 10:53:22.351Z | 121.806° 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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