STARLINK-32573, 61725
Orbit data source: Space-Track
STARLINK-32573, 61725 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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61725 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: 1 day ago
TLE from 1 day ago
0 STARLINK-32573
1 61725U 24196U 25312.26327143 .00000438 00000-0 26921-4 0 9993
2 61725 53.1614 305.5008 0001436 93.1114 267.0051 15.30195564 58561Epoch: 2025-11-08T06:19Z
TLE epoch observation values (Epoch: 2025-11-08T06:19:06.651Z)
Latitude
-0.00003°
Longitude
163.02767°
Altitude
476.18 km
Speed
7.629 km/s
True Right ascension
20h 22m 00s
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
12:02:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.469 km
Perigee altitude
474.5 km
Semi-major axis
6,853.622 km
Eccentricity
0.00014
Inclination
53.1614°
RAAN
305.5008°
Arg. of periapsis
93.1114°
True anomaly
266.98867°
Mean anomaly
267.0051°
Eccentric anomaly
266.99688°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000026921
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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-32573 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 | 2025-11-10 00:47:28.587Z | 167.192° S | 2025-11-10 00:49:28.587Z | 133.725° SE | 15.699° | 2025-11-10 00:51:28.587Z | 96.177° ESE |
| 5 mins | 2025-11-10 02:25:28.587Z | 253.332° W | 2025-11-10 02:27:28.587Z | 333.918° NNW | 39.741° | 2025-11-10 02:30:28.587Z | 41.419° NE |
| 4 mins | 2025-11-10 07:22:28.587Z | 348.572° N | 2025-11-10 07:24:28.587Z | 32.23° NE | 19.629° | 2025-11-10 07:26:28.587Z | 69.88° E |
| 5 mins | 2025-11-10 09:00:28.587Z | 299.561° NW | 2025-11-10 09:02:28.587Z | 210.286° SW | 42.703° | 2025-11-10 09:05:28.587Z | 141.054° SSE |
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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