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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-32486
1 61854U 24202K 25319.61262343 -.00001310 00000-0 -38136-4 0 9993
2 61854 43.0023 162.0153 0001714 262.2948 97.7709 15.27545659 57899Epoch: 2025-11-15T14:42Z
TLE epoch observation values (Epoch: 2025-11-15T14:42:10.664Z)
Latitude
-0.00001°
Longitude
-113.46841°
Altitude
483.087 km
Speed
7.626 km/s
True Right ascension
10h 48m 03s
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
09:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.273 km
Perigee altitude
483.92 km
Semi-major axis
6,863.234 km
Eccentricity
0.00017
Inclination
43.0023°
RAAN
162.0153°
Arg. of periapsis
262.2948°
True anomaly
97.79036°
Mean anomaly
97.7709°
Eccentric anomaly
97.78063°
Mean motion
3.81724 °/min
Orbital period
94.31 mins
BSTAR
-0.000038136
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-16 15:59:28.708Z | 187.979° SSW | 2025-11-16 16:02:28.708Z | 133.499° SE | 17.474° | 2025-11-16 16:04:28.708Z | 100.316° ESE |
| 5 mins | 2025-11-16 17:38:28.708Z | 243.288° WSW | 2025-11-16 17:40:28.708Z | 183.24° SSW | 44.399° | 2025-11-16 17:43:28.708Z | 73.833° E |
| 5 mins | 2025-11-16 19:17:28.708Z | 287.407° WNW | 2025-11-16 19:19:28.708Z | 343.935° N | 38.026° | 2025-11-16 19:22:28.708Z | 70.784° E |
| 6 mins | 2025-11-16 20:56:28.708Z | 292.092° WNW | 2025-11-16 20:58:28.708Z | 324.635° NNW | 42.257° | 2025-11-16 21:02:28.708Z | 100.376° ESE |
| 5 mins | 2025-11-16 22:35:28.708Z | 263.761° W | 2025-11-16 22:37:28.708Z | 217.021° SW | 27.564° | 2025-11-16 22:40:28.708Z | 151.446° 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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