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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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-32540
1 61723U 24196S 26283.35174873 .00000895 00000-0 37641-4 0 9997
2 61723 53.1597 144.5582 0001547 85.3385 274.7794 15.34393705110573Epoch: 2026-10-10T08:26Z
TLE epoch observation values (Epoch: 2026-10-10T08:26:31.090Z)
Latitude
-0.00003°
Longitude
-1.03148°
Altitude
463.535 km
Speed
7.636 km/s
True Right ascension
09h 38m 13s
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
08:34:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.037 km
Perigee altitude
461.921 km
Semi-major axis
6,841.116 km
Eccentricity
0.00015
Inclination
53.1597°
RAAN
144.5582°
Arg. of periapsis
85.3385°
True anomaly
274.76173°
Mean anomaly
274.7794°
Eccentric anomaly
274.77057°
Mean motion
3.83577 °/min
Orbital period
93.85 mins
BSTAR
0.000037641
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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 | 2026-10-11 17:27:36.681Z | 232.741° WSW | 2026-10-11 17:30:36.681Z | 31.956° NE | 67.099° | 2026-10-11 17:33:36.681Z | 48.395° ENE |
| 6 mins | 2026-10-12 00:01:36.681Z | 314.065° NW | 2026-10-12 00:04:36.681Z | 102.64° ESE | 64.338° | 2026-10-12 00:07:36.681Z | 126.256° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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