STARLINK-32201, 61512
Orbit data source: Space-Track
STARLINK-32201, 61512 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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61512 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-32201
1 61512U 24183D 25346.82281747 -.00000385 00000-0 -88787-6 0 9994
2 61512 53.1601 173.0905 0001263 107.9733 252.1406 15.30183425 66532Epoch: 2025-12-12T19:44Z
TLE epoch observation values (Epoch: 2025-12-12T19:44:51.429Z)
Latitude
0.00002°
Longitude
155.11731°
Altitude
476.43 km
Speed
7.629 km/s
True Right ascension
11h 32m 21s
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
09:16:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.387 km
Perigee altitude
474.655 km
Semi-major axis
6,853.658 km
Eccentricity
0.00013
Inclination
53.1601°
RAAN
173.0905°
Arg. of periapsis
107.9733°
True anomaly
252.12683°
Mean anomaly
252.1406°
Eccentric anomaly
252.13371°
Mean motion
3.82525 °/min
Orbital period
94.11 mins
BSTAR
-8.8787e-7
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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-32201 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 14:43:21.388Z | 198.295° SSW | 2025-12-13 14:46:21.388Z | 120.006° SE | 31.681° | 2025-12-13 14:49:21.388Z | 64.716° ENE |
| 4 mins | 2025-12-13 16:22:21.388Z | 287.521° WNW | 2025-12-13 16:24:21.388Z | 341.147° N | 25.119° | 2025-12-13 16:26:21.388Z | 23.499° NE |
| 4 mins | 2025-12-13 21:19:21.388Z | 342.909° N | 2025-12-13 21:21:21.388Z | 49.094° ENE | 30.032° | 2025-12-13 21:23:21.388Z | 93.406° ESE |
| 4 mins | 2025-12-13 22:57:21.388Z | 265.533° W | 2025-12-13 22:58:21.388Z | 240.851° WSW | 24.004° | 2025-12-13 23:01:21.388Z | 174.799° 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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