STARLINK-32156, 60278
Orbit data source: Space-Track
STARLINK-32156, 60278 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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60278 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32156
1 60278U 24132A 25307.64534341 -.00006568 00000-0 -21024-3 0 9991
2 60278 53.1606 277.8107 0001278 101.8150 258.2994 15.30137210 73486Epoch: 2025-11-03T15:29Z
TLE epoch observation values (Epoch: 2025-11-03T15:29:17.670Z)
Latitude
-0.00004°
Longitude
2.3433°
Altitude
476.48 km
Speed
7.629 km/s
True Right ascension
18h 31m 14s
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
00:05:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.535 km
Perigee altitude
474.783 km
Semi-major axis
6,853.796 km
Eccentricity
0.00013
Inclination
53.1606°
RAAN
277.8107°
Arg. of periapsis
101.815°
True anomaly
258.28506°
Mean anomaly
258.2994°
Eccentric anomaly
258.29223°
Mean motion
3.82513 °/min
Orbital period
94.11 mins
BSTAR
-0.00021024
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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-32156 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 | 2025-11-04 07:40:47.833Z | 315.276° NNW | 2025-11-04 07:42:47.833Z | 63.321° ENE | 44.383° | 2025-11-04 07:45:47.833Z | 126.177° SE |
| 6 mins | 2025-11-05 00:35:47.833Z | 224.734° SW | 2025-11-05 00:37:47.833Z | 207.973° SW | 42.856° | 2025-11-05 00:41:47.833Z | 51.692° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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