STARLINK-32484, 62160
Orbit data source: Space-Track
STARLINK-32484, 62160 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 30 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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62160 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-32484
1 62160U 24224X 25348.20938419 .00027541 00000-0 10071-2 0 9997
2 62160 43.0029 281.1321 0001512 270.8849 89.1829 15.27563418 59407Epoch: 2025-12-14T05:01Z
TLE epoch observation values (Epoch: 2025-12-14T05:01:30.794Z)
Latitude
-0.00003°
Longitude
122.62818°
Altitude
482.86 km
Speed
7.626 km/s
True Right ascension
18h 44m 31s
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
15:09:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.081 km
Perigee altitude
484.006 km
Semi-major axis
6,863.18 km
Eccentricity
0.00015
Inclination
43.0029°
RAAN
281.1321°
Arg. of periapsis
270.8849°
True anomaly
89.20022°
Mean anomaly
89.1829°
Eccentric anomaly
89.19156°
Mean motion
3.81729 °/min
Orbital period
94.31 mins
BSTAR
0.0010071
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Other satellites on launch #224 in the year 2024 (2024-11-30 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-32484 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 | 2025-12-15 22:01:16.560Z | 190.796° SSW | 2025-12-15 22:03:16.560Z | 150.179° SSE | 21.774° | 2025-12-15 22:06:16.560Z | 93.479° ESE |
| 5 mins | 2025-12-15 23:40:16.560Z | 252.929° W | 2025-12-15 23:42:16.560Z | 58.246° ENE | 44.585° | 2025-12-15 23:45:16.560Z | 71.572° E |
| 5 mins | 2025-12-16 01:19:16.560Z | 293.066° NW | 2025-12-16 01:21:16.560Z | 2.485° NNE | 37.975° | 2025-12-16 01:24:16.560Z | 74.405° E |
| 5 mins | 2025-12-16 02:58:16.560Z | 290.116° WNW | 2025-12-16 03:00:16.560Z | 333.508° NNW | 44.714° | 2025-12-16 03:03:16.560Z | 105.673° ESE |
| 4 mins | 2025-12-16 04:37:16.560Z | 254.425° W | 2025-12-16 04:39:16.560Z | 207.588° SW | 22.997° | 2025-12-16 04:41:16.560Z | 166.272° S |
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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