STARLINK-32143, 60296
Orbit data source: Space-Track
STARLINK-32143, 60296 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 Jul 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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60296 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: 7 hours ago
TLE from 7 hours ago
0 STARLINK-32143
1 60296U 24132U 26026.60432337 .00022709 00000-0 77635-3 0 9990
2 60296 53.1583 248.1473 0000469 61.0878 299.0170 15.30205838 85116Epoch: 2026-01-26T14:30Z
TLE epoch observation values (Epoch: 2026-01-26T14:30:13.539Z)
Latitude
0.00002°
Longitude
-95.30679°
Altitude
475.941 km
Speed
7.629 km/s
True Right ascension
16h 32m 35s
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
23:22:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.776 km
Perigee altitude
475.133 km
Semi-major axis
6,853.591 km
Eccentricity
0.00005
Inclination
53.1583°
RAAN
248.1473°
Arg. of periapsis
61.0878°
True anomaly
299.0123°
Mean anomaly
299.017°
Eccentric anomaly
299.01465°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00077635
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Other satellites on launch #132 in the year 2024 (2024-07-28 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-32143 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-26 22:47:25.527Z | 344.545° N | 2026-01-26 22:49:25.527Z | 23.169° NE | 17.893° | 2026-01-26 22:51:25.527Z | 61.44° ENE |
| 5 mins | 2026-01-27 00:25:25.527Z | 308.589° NW | 2026-01-27 00:27:25.527Z | 295.77° NW | 43.91° | 2026-01-27 00:30:25.527Z | 133.002° SE |
| 5 mins | 2026-01-27 17:21:25.527Z | 234.291° WSW | 2026-01-27 17:23:25.527Z | 26.501° NE | 43.725° | 2026-01-27 17:26:25.527Z | 48.473° ENE |
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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