STARLINK-32012, 60027
Orbit data source: Space-Track
STARLINK-32012, 60027 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Jun 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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60027 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: 3 days ago
TLE from 3 days ago
0 STARLINK-32012
1 60027U 24111M 26170.82928342 .00003563 00000-0 13229-3 0 9995
2 60027 53.1625 321.0429 0001186 82.4132 277.7004 15.30222074114678Epoch: 2026-06-19T19:54Z
TLE epoch observation values (Epoch: 2026-06-19T19:54:10.087Z)
Latitude
0.00002°
Longitude
114.44824°
Altitude
475.94 km
Speed
7.629 km/s
True Right ascension
21h 24m 10s
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
21:29:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.218 km
Perigee altitude
474.592 km
Semi-major axis
6,853.542 km
Eccentricity
0.00012
Inclination
53.1625°
RAAN
321.0429°
Arg. of periapsis
82.4132°
True anomaly
277.68693°
Mean anomaly
277.7004°
Eccentric anomaly
277.69367°
Mean motion
3.82534 °/min
Orbital period
94.11 mins
BSTAR
0.00013229
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Other satellites on launch #111 in the year 2024 (2024-06-08 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-32012 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 | 2026-06-22 12:22:54.872Z | 248.765° W | 2026-06-22 12:24:54.872Z | 330.427° NNW | 41.318° | 2026-06-22 12:27:54.872Z | 42.678° NE |
| 4 mins | 2026-06-22 17:19:54.872Z | 348.482° N | 2026-06-22 17:21:54.872Z | 30.797° NE | 18.869° | 2026-06-22 17:23:54.872Z | 67.836° E |
| 5 mins | 2026-06-22 18:57:54.872Z | 303.138° NW | 2026-06-22 18:59:54.872Z | 213.912° SW | 43.927° | 2026-06-22 19:02:54.872Z | 137.969° 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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