STARLINK-32540, 61723
Orbit data source: Space-Track
STARLINK-32540, 61723 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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61723 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32540
1 61723U 24196S 25286.66932593 -.00000374 00000-0 -51012-6 0 9998
2 61723 53.1602 28.4229 0001021 115.8931 244.2175 15.30188774 55141Epoch: 2025-10-13T16:03Z
TLE epoch observation values (Epoch: 2025-10-13T16:03:49.760Z)
Latitude
-0.00002°
Longitude
124.99676°
Altitude
476.453 km
Speed
7.629 km/s
True Right ascension
01h 53m 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
23:08:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.205 km
Perigee altitude
474.805 km
Semi-major axis
6,853.642 km
Eccentricity
0.0001
Inclination
53.1602°
RAAN
28.4229°
Arg. of periapsis
115.8931°
True anomaly
244.20697°
Mean anomaly
244.2175°
Eccentric anomaly
244.21223°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-5.1012e-7
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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-32540 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 | 2025-10-14 09:28:38.273Z | 221.007° SW | 2025-10-14 09:31:38.273Z | 173.083° S | 42.769° | 2025-10-14 09:34:38.273Z | 55.5° ENE |
| 4 mins | 2025-10-14 11:08:38.273Z | 303.491° NW | 2025-10-14 11:09:38.273Z | 324.074° NNW | 18.949° | 2025-10-14 11:12:38.273Z | 22.697° NE |
| 5 mins | 2025-10-14 16:04:38.273Z | 321.887° NNW | 2025-10-14 16:06:38.273Z | 11.376° NNE | 39.905° | 2025-10-14 16:09:38.273Z | 114.604° 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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