STARLINK-32509, 62042
Orbit data source: Space-Track
STARLINK-32509, 62042 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 21 Nov 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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62042 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: 18 hours ago
TLE from 18 hours ago
0 STARLINK-32509
1 62042U 24216L 25312.45250700 .00029375 00000-0 10711-2 0 9993
2 62042 43.0012 221.0387 0001728 263.5581 96.5074 15.27629004 55330Epoch: 2025-11-08T10:51Z
TLE epoch observation values (Epoch: 2025-11-08T10:51:36.604Z)
Latitude
-0.00003°
Longitude
10.25424°
Altitude
482.812 km
Speed
7.626 km/s
True Right ascension
14h 44m 09s
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
00:42:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.033 km
Perigee altitude
483.661 km
Semi-major axis
6,862.984 km
Eccentricity
0.00017
Inclination
43.0012°
RAAN
221.0387°
Arg. of periapsis
263.5581°
True anomaly
96.52707°
Mean anomaly
96.5074°
Eccentric anomaly
96.51724°
Mean motion
3.81745 °/min
Orbital period
94.3 mins
BSTAR
0.0010711
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Other satellites on launch #216 in the year 2024 (2024-11-21 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-32509 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 | 2025-11-09 21:37:21.018Z | 234.674° WSW | 2025-11-09 21:40:21.018Z | 113.202° SE | 39.916° | 2025-11-09 21:43:21.018Z | 75.469° E |
| 6 mins | 2025-11-09 23:16:21.018Z | 280.393° WNW | 2025-11-09 23:19:21.018Z | 24.941° NE | 37.486° | 2025-11-09 23:22:21.018Z | 72.082° E |
| 5 mins | 2025-11-10 00:56:21.018Z | 298.104° NW | 2025-11-10 00:58:21.018Z | 38.823° NE | 41.508° | 2025-11-10 01:01:21.018Z | 93.662° ESE |
| 5 mins | 2025-11-10 02:35:21.018Z | 260.684° W | 2025-11-10 02:37:21.018Z | 190.931° SSW | 32.051° | 2025-11-10 02:40:21.018Z | 138.901° 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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