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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-32156
1 60278U 24132A 25308.10248595 .00003139 00000-0 11805-3 0 9991
2 60278 53.1625 275.6865 0001018 99.1853 260.9262 15.30207457 73552Epoch: 2025-11-04T02:27Z
TLE epoch observation values (Epoch: 2025-11-04T02:27:34.786Z)
Latitude
-0.00008°
Longitude
-164.80283°
Altitude
476.203 km
Speed
7.629 km/s
True Right ascension
18h 22m 44s
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
04:05:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.147 km
Perigee altitude
474.751 km
Semi-major axis
6,853.586 km
Eccentricity
0.0001
Inclination
53.1625°
RAAN
275.6865°
Arg. of periapsis
99.1853°
True anomaly
260.91468°
Mean anomaly
260.9262°
Eccentric anomaly
260.92044°
Mean motion
3.82531 °/min
Orbital period
94.11 mins
BSTAR
0.00011805
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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 | 2025-11-05 00:35:49.092Z | 224.224° SW | 2025-11-05 00:37:49.092Z | 188.718° SSW | 44.268° | 2025-11-05 00:40:49.092Z | 52.321° ENE |
| 4 mins | 2025-11-05 02:14:49.092Z | 306.086° NW | 2025-11-05 02:15:49.092Z | 325.995° NNW | 17.902° | 2025-11-05 02:18:49.092Z | 22.571° NE |
| 5 mins | 2025-11-05 07:10:49.092Z | 318.925° NNW | 2025-11-05 07:12:49.092Z | 9.389° NNE | 42.095° | 2025-11-05 07:15:49.092Z | 119.538° SE |
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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