STARLINK-32141, 60290
Orbit data source: Space-Track
STARLINK-32141, 60290 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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60290 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-32141
1 60290U 24132N 25321.03904107 -.00000838 00000-0 -16163-4 0 9998
2 60290 53.1613 215.6431 0001542 89.7237 270.3941 15.30195042 74319Epoch: 2025-11-17T00:56Z
TLE epoch observation values (Epoch: 2025-11-17T00:56:13.148Z)
Latitude
0.00002°
Longitude
145.24313°
Altitude
476.123 km
Speed
7.629 km/s
True Right ascension
14h 22m 34s
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
19:19:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.543 km
Perigee altitude
474.429 km
Semi-major axis
6,853.623 km
Eccentricity
0.00015
Inclination
53.1613°
RAAN
215.6431°
Arg. of periapsis
89.7237°
True anomaly
270.37643°
Mean anomaly
270.3941°
Eccentric anomaly
270.38527°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
-0.000016163
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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-32141 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 | 2025-11-18 02:32:11.475Z | 314.433° NW | 2025-11-18 02:34:11.475Z | 94.675° ESE | 44.108° | 2025-11-18 02:37:11.475Z | 127.49° SE |
| 5 mins | 2025-11-18 19:27:11.475Z | 226.001° WSW | 2025-11-18 19:29:11.475Z | 204.439° SW | 44.272° | 2025-11-18 19:32:11.475Z | 51.495° ENE |
| 4 mins | 2025-11-18 21:06:11.475Z | 305.867° NW | 2025-11-18 21:08:11.475Z | 347.68° N | 17.622° | 2025-11-18 21:10:11.475Z | 21.919° NNE |
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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