STARLINK-32260, 61522
Orbit data source: Space-Track
STARLINK-32260, 61522 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 15 Oct 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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61522 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32260
1 61522U 24183P 25346.93500109 .00002018 00000-0 80306-4 0 9993
2 61522 53.1603 185.1412 0001373 91.4141 268.7017 15.30177184 66372Epoch: 2025-12-12T22:26Z
TLE epoch observation values (Epoch: 2025-12-12T22:26:24.094Z)
Latitude
-0.00001°
Longitude
126.67131°
Altitude
476.204 km
Speed
7.629 km/s
True Right ascension
12h 20m 33s
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
07:31:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.481 km
Perigee altitude
474.599 km
Semi-major axis
6,853.677 km
Eccentricity
0.00014
Inclination
53.1603°
RAAN
185.1412°
Arg. of periapsis
91.4141°
True anomaly
268.68597°
Mean anomaly
268.7017°
Eccentric anomaly
268.69384°
Mean motion
3.82523 °/min
Orbital period
94.11 mins
BSTAR
0.000080306
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Other satellites on launch #183 in the year 2024 (2024-10-15 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-32260 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 | 2025-12-13 15:51:16.803Z | 214.8° SW | 2025-12-13 15:54:16.803Z | 130.341° SE | 41.071° | 2025-12-13 15:57:16.803Z | 57.911° ENE |
| 4 mins | 2025-12-13 17:31:16.803Z | 308.023° NW | 2025-12-13 17:32:16.803Z | 331.769° NNW | 20.752° | 2025-12-13 17:35:16.803Z | 27.353° NE |
| 5 mins | 2025-12-13 22:27:16.803Z | 328.618° NNW | 2025-12-13 22:29:16.803Z | 38.932° NE | 38.083° | 2025-12-13 22:32:16.803Z | 111.247° ESE |
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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