View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 06393U 26022.33450664 +.00000000 +00000-0 +17428-3 0 00002
2 06393 81.2572 159.8689 0059054 91.5519 269.2415 14.05418384 04
| Epoch (UTC): | 22 January 2026 08:01:41 |
| Eccentricity: | 0.0059054 |
| inclination: | 81.2572° |
| perigee height: | 832 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 159.8689° |
| argument of perigee: | 91.5519° |
| revolutions per day: | 14.05418384 |
| mean anomaly at epoch: | 269.2415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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