KOREASAT 5, 29349
Orbit data source: Space-Track
KOREASAT 5, 29349 is a South Korean payload satellite in GEO that was launched on Tue, 22 Aug 2006 UTC via a ZENIT-3SL launch vehicle from the Sea Launch (SEAL). 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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29349 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 23 hours ago
0 KOREASAT 5
1 29349U 06034A 25235.85183635 -.00000373 00000-0 00000-0 0 9990
2 29349 1.0105 87.2843 0001648 112.3368 192.4724 1.00272466 38335
Epoch: 2025-08-23T20:26Z
TLE epoch observation values (Epoch: 2025-08-23T20:26:38.66Z)
Latitude
-0.85609°
Longitude
113.0653°
Altitude
35,792.782 km
Speed
3.074 km/s
True Right ascension
02h 08m 25s
True Declination
0° 51' 19"
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
11:03:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,794.423 km
Perigee altitude
35,780.525 km
Semi-major axis
42,165.611 km
Eccentricity
0.00016
Inclination
1.0105°
RAAN
87.2843°
Arg. of periapsis
112.3368°
True anomaly
192.46832°
Mean anomaly
192.4724°
Eccentric anomaly
192.47036°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #34 in the year 2006 (2006-08-22 UTC)
KOREASAT 5 Visibility
Observer location: undefined°, undefined°
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. |
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29349 neighbors
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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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