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: 2 days ago
TLE from 2 days ago
0 STARLINK-32156
1 60278U 24132A 25322.01454416 .00000484 00000-0 28485-4 0 9991
2 60278 53.1606 211.0663 0001125 91.7911 268.3219 15.30173038 75680Epoch: 2025-11-18T00:20Z
TLE epoch observation values (Epoch: 2025-11-18T00:20:56.615Z)
Latitude
0.00001°
Longitude
148.5237°
Altitude
476.218 km
Speed
7.629 km/s
True Right ascension
14h 04m 15s
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
13:49:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.323 km
Perigee altitude
474.781 km
Semi-major axis
6,853.689 km
Eccentricity
0.00011
Inclination
53.1606°
RAAN
211.0663°
Arg. of periapsis
91.7911°
True anomaly
268.30901°
Mean anomaly
268.3219°
Eccentric anomaly
268.31546°
Mean motion
3.82522 °/min
Orbital period
94.11 mins
BSTAR
0.000028485
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-19 18:50:22.326Z | 216.753° SW | 2025-11-19 18:53:22.326Z | 164.526° S | 40.676° | 2025-11-19 18:56:22.326Z | 58.733° ENE |
| 4 mins | 2025-11-19 20:30:22.326Z | 301.254° NW | 2025-11-19 20:31:22.326Z | 322.735° NNW | 20.109° | 2025-11-19 20:34:22.326Z | 23.278° NE |
| 5 mins | 2025-11-20 01:26:22.326Z | 324.687° NNW | 2025-11-20 01:28:22.326Z | 14.191° NNE | 37.68° | 2025-11-20 01:31:22.326Z | 109.959° ESE |
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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