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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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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-32156
1 60278U 24132A 26137.60989690 -.00000581 00000-0 -74956-5 0 9993
2 60278 53.1605 92.2142 0001316 83.3974 276.7177 15.30186801103330Epoch: 2026-05-17T14:38Z
TLE epoch observation values (Epoch: 2026-05-17T14:38:15.092Z)
Latitude
0.00003°
Longitude
-2.6587°
Altitude
476.049 km
Speed
7.629 km/s
True Right ascension
06h 08m 51s
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
08:10:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.413 km
Perigee altitude
474.609 km
Semi-major axis
6,853.648 km
Eccentricity
0.00013
Inclination
53.1605°
RAAN
92.2142°
Arg. of periapsis
83.3974°
True anomaly
276.70272°
Mean anomaly
276.7177°
Eccentric anomaly
276.71021°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.0000074956
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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 | 2026-05-18 00:14:43.497Z | 248.406° W | 2026-05-18 00:17:43.497Z | 348.908° N | 38.396° | 2026-05-18 00:20:43.497Z | 41.879° NE |
| 4 mins | 2026-05-18 05:12:43.497Z | 352.049° N | 2026-05-18 05:13:43.497Z | 13.076° NNE | 19.6° | 2026-05-18 05:16:43.497Z | 73° E |
| 5 mins | 2026-05-18 06:50:43.497Z | 296.827° NW | 2026-05-18 06:52:43.497Z | 189.623° SSW | 41.368° | 2026-05-18 06:55:43.497Z | 141.482° SSE |
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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