STARLINK-32486, 61854
Orbit data source: Space-Track
STARLINK-32486, 61854 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 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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61854 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: 1 day ago
TLE from 1 day ago
0 STARLINK-32486
1 61854U 24202K 25305.55451841 .00001305 00000-0 56950-4 0 9990
2 61854 43.0047 241.4087 0001449 260.7405 99.3283 15.27579086 55747Epoch: 2025-11-01T13:18Z
TLE epoch observation values (Epoch: 2025-11-01T13:18:30.390Z)
Latitude
-0.00002°
Longitude
0.69913°
Altitude
482.989 km
Speed
7.626 km/s
True Right ascension
16h 05m 38s
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
19:32:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.991 km
Perigee altitude
484.002 km
Semi-major axis
6,863.133 km
Eccentricity
0.00014
Inclination
43.0047°
RAAN
241.4087°
Arg. of periapsis
260.7405°
True anomaly
99.34468°
Mean anomaly
99.3283°
Eccentric anomaly
99.33649°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.00005695
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Other satellites on launch #202 in the year 2024 (2024-11-07 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-32486 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 | 2025-11-03 00:05:53.149Z | 256.287° W | 2025-11-03 00:08:53.149Z | 15.085° NNE | 44.504° | 2025-11-03 00:11:53.149Z | 70.631° E |
| 5 mins | 2025-11-03 01:45:53.149Z | 293.486° NW | 2025-11-03 01:47:53.149Z | 357.217° N | 38° | 2025-11-03 01:50:53.149Z | 75.469° E |
| 5 mins | 2025-11-03 03:24:53.149Z | 287.929° WNW | 2025-11-03 03:26:53.149Z | 282.03° WNW | 44.563° | 2025-11-03 03:29:53.149Z | 109.814° ESE |
| 4 mins | 2025-11-03 05:03:53.149Z | 253.123° W | 2025-11-03 05:05:53.149Z | 210.346° SW | 20.61° | 2025-11-03 05:07:53.149Z | 171.174° S |
| 4 mins | 2025-11-03 22:00:53.149Z | 182.988° SSW | 2025-11-03 22:01:53.149Z | 159.53° S | 23.336° | 2025-11-03 22:04:53.149Z | 94.853° ESE |
| 4 mins | 2025-11-03 23:38:53.149Z | 256.676° W | 2025-11-03 23:40:53.149Z | 299.151° NW | 44.492° | 2025-11-03 23:42:53.149Z | 68.679° E |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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