STARLINK-32744, 62509
Orbit data source: Space-Track
STARLINK-32744, 62509 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 Jan 2025 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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62509 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: 19 hours ago
TLE from 19 hours ago
0 STARLINK-32744
1 62509U 25003Y 26171.05599061 .00015889 00000-0 58529-3 0 9997
2 62509 43.0024 71.1658 0001402 277.9868 82.0825 15.27602347 82203Epoch: 2026-06-20T01:20Z
TLE epoch observation values (Epoch: 2026-06-20T01:20:37.588Z)
Latitude
0°
Longitude
142.73309°
Altitude
482.626 km
Speed
7.626 km/s
True Right ascension
04h 44m 39s
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
07:16:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.889 km
Perigee altitude
483.965 km
Semi-major axis
6,863.064 km
Eccentricity
0.00014
Inclination
43.0024°
RAAN
71.1658°
Arg. of periapsis
277.9868°
True anomaly
82.09841°
Mean anomaly
82.0825°
Eccentric anomaly
82.09046°
Mean motion
3.81739 °/min
Orbital period
94.31 mins
BSTAR
0.00058529
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Other satellites on launch #3 in the year 2025 (2025-01-06 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-32744 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 | 2026-06-20 20:22:06.091Z | 209.493° SW | 2026-06-20 20:25:06.091Z | 150.033° SSE | 27.139° | 2026-06-20 20:28:06.091Z | 88.53° E |
| 5 mins | 2026-06-20 22:02:06.091Z | 264.073° W | 2026-06-20 22:04:06.091Z | 17.222° NNE | 43.56° | 2026-06-20 22:07:06.091Z | 70.09° E |
| 5 mins | 2026-06-20 23:41:06.091Z | 295.432° NW | 2026-06-20 23:43:06.091Z | 3.259° NNE | 38.242° | 2026-06-20 23:46:06.091Z | 77.79° E |
| 5 mins | 2026-06-21 01:20:06.091Z | 285.212° WNW | 2026-06-21 01:22:06.091Z | 227.904° WSW | 44.525° | 2026-06-21 01:25:06.091Z | 114.402° SE |
| 4 mins | 2026-06-21 02:59:06.091Z | 248.979° W | 2026-06-21 03:01:06.091Z | 208.528° SW | 18.057° | 2026-06-21 03:03:06.091Z | 173.522° S |
| 5 mins | 2026-06-21 19:55:06.091Z | 200.618° SSW | 2026-06-21 19:57:06.091Z | 156.497° SSE | 26.386° | 2026-06-21 20:00:06.091Z | 90.769° ESE |
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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