KOMPSAT 2, 29268
Orbit data source: Space-Track
KOMPSAT 2, 29268 is a payload satellite owned by KARI (KR) in SSO that was launched on Fri, 28 Jul 2006 UTC via an ROKOT launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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29268 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
KARI
Mission
Operational Civil Imaging
Bus & Motor
KOMPSAT, Unknown motor
Mass
765 kg wet, 692 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.5 m
Radar Cross Section
9.840 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 KOMPSAT 2
1 29268U 06031A 26106.34084611 .00000061 00000-0 19894-4 0 9991
2 29268 97.8309 293.7782 0012983 270.5364 212.6015 14.64619959 52427Epoch: 2026-04-16T08:10Z
TLE epoch observation values (Epoch: 2026-04-16T08:10:49.103Z)
Latitude
56.23135°
Longitude
158.38877°
Altitude
695.411 km
Speed
7.51 km/s
True Right ascension
08h 22m 19s
True Declination
56° 04' 15"
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
02:32:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
684.512 km
Perigee altitude
666.197 km
Semi-major axis
7,053.491 km
Eccentricity
0.0013
Inclination
97.8309°
RAAN
293.7782°
Arg. of periapsis
270.5364°
True anomaly
212.52145°
Mean anomaly
212.6015°
Eccentric anomaly
212.56146°
Mean motion
3.66384 °/min
Orbital period
98.26 mins
BSTAR
0.000019894
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Other satellites on launch #31 in the year 2006 (2006-07-28 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.KOMPSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-17 00:36:24.970Z | 41.695° NE | 2026-04-17 00:39:24.970Z | 93.262° ESE | 26.776° | 2026-04-17 00:43:24.970Z | 156.706° SSE |
| 6 mins | 2026-04-17 02:14:24.970Z | 332.475° NNW | 2026-04-17 02:16:24.970Z | 297.627° NW | 23.43° | 2026-04-17 02:20:24.970Z | 236.934° WSW |
| 5 mins | 2026-04-17 11:39:24.970Z | 106.876° ESE | 2026-04-17 11:41:24.970Z | 67.707° E | 24.878° | 2026-04-17 11:44:24.970Z | 18.035° NNE |
| 6 mins | 2026-04-17 13:16:24.970Z | 222.578° SW | 2026-04-17 13:18:24.970Z | 260.755° W | 25.293° | 2026-04-17 13:22:24.970Z | 322.902° NNW |
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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