STARLINK-32408, 62054
Orbit data source: Space-Track
STARLINK-32408, 62054 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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62054 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-32408
1 62054U 24216Y 26040.10381547 .00027244 00000-0 99565-3 0 9999
2 62054 43.0031 57.7725 0001443 234.0574 126.0144 15.27588135 69514Epoch: 2026-02-09T02:29Z
TLE epoch observation values (Epoch: 2026-02-09T02:29:29.656Z)
Latitude
-0.00002°
Longitude
-118.80452°
Altitude
483.383 km
Speed
7.625 km/s
True Right ascension
03h 51m 05s
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
10:50:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.96 km
Perigee altitude
483.979 km
Semi-major axis
6,863.106 km
Eccentricity
0.00014
Inclination
43.0031°
RAAN
57.7725°
Arg. of periapsis
234.0574°
True anomaly
126.02777°
Mean anomaly
126.0144°
Eccentric anomaly
126.02109°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.00099565
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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-32408 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-10 08:43:29.095Z | 288.035° WNW | 2026-02-10 08:47:29.095Z | 108.382° ESE | 43.833° | 2026-02-10 08:50:29.095Z | 109.135° ESE |
| 4 mins | 2026-02-10 10:24:29.095Z | 244.71° WSW | 2026-02-10 10:25:29.095Z | 222.43° SW | 20.856° | 2026-02-10 10:28:29.095Z | 164.35° S |
| 4 mins | 2026-02-11 03:20:29.095Z | 189.356° SSW | 2026-02-11 03:22:29.095Z | 142.955° SSE | 23.317° | 2026-02-11 03:24:29.095Z | 100.352° ESE |
| 6 mins | 2026-02-11 04:58:29.095Z | 255.139° W | 2026-02-11 05:01:29.095Z | 57.04° ENE | 42.633° | 2026-02-11 05:04:29.095Z | 71.251° E |
| 5 mins | 2026-02-11 06:38:29.095Z | 297.164° NW | 2026-02-11 06:40:29.095Z | 19.495° NNE | 37.344° | 2026-02-11 06:43:29.095Z | 76.608° E |
| 5 mins | 2026-02-11 08:17:29.095Z | 288.966° WNW | 2026-02-11 08:19:29.095Z | 97.702° ESE | 44.684° | 2026-02-11 08:22:29.095Z | 108.292° 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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