STARLINK-32022, 60149
Orbit data source: Space-Track
STARLINK-32022, 60149 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 27 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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60149 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-32022
1 60149U 24120Q 26171.36118124 -.00001370 00000-0 -29431-4 0 9998
2 60149 53.1593 202.4589 0000938 84.4660 275.6449 15.34384573112189Epoch: 2026-06-20T08:40Z
TLE epoch observation values (Epoch: 2026-06-20T08:40:06.059Z)
Latitude
-0.00005°
Longitude
163.85671°
Altitude
463.587 km
Speed
7.636 km/s
True Right ascension
13h 29m 50s
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
07:13:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.648 km
Perigee altitude
462.364 km
Semi-major axis
6,841.143 km
Eccentricity
0.00009
Inclination
53.1593°
RAAN
202.4589°
Arg. of periapsis
84.466°
True anomaly
275.6342°
Mean anomaly
275.6449°
Eccentric anomaly
275.63955°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
-0.000029431
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Other satellites on launch #120 in the year 2024 (2024-06-27 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-32022 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 | 2026-06-21 05:12:36.192Z | 257.232° W | 2026-06-21 05:14:36.192Z | 354.007° N | 37.945° | 2026-06-21 05:17:36.192Z | 42.414° NE |
| 5 mins | 2026-06-21 10:07:36.192Z | 336.525° NNW | 2026-06-21 10:10:36.192Z | 35.361° NE | 18.929° | 2026-06-21 10:12:36.192Z | 71.478° E |
| 6 mins | 2026-06-21 11:45:36.192Z | 302.823° NW | 2026-06-21 11:47:36.192Z | 272.669° WNW | 40.281° | 2026-06-21 11:51:36.192Z | 139.744° 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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