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 26129.26517567 +.00000000 +00000-0 +95773-4 0 00008
2 06393 81.2570 56.7092 0058759 150.2721 210.1808 14.05435735 04
| Epoch (UTC): | 09 May 2026 06:21:51 |
| Eccentricity: | 0.0058759 |
| inclination: | 81.2570° |
| perigee height: | 832 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 56.7092° |
| argument of perigee: | 150.2721° |
| revolutions per day: | 14.05435735 |
| mean anomaly at epoch: | 210.1808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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