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 13068U 26070.81834160 +.00000000 +00000-0 +18360-3 0 00008
2 13068 81.1759 158.2762 0022717 170.3530 189.8143 15.22040884 08
| Epoch (UTC): | 11 March 2026 19:38:24 |
| Eccentricity: | 0.0022717 |
| inclination: | 81.1759° |
| perigee height: | 484 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 158.2762° |
| argument of perigee: | 170.3530° |
| revolutions per day: | 15.22040884 |
| mean anomaly at epoch: | 189.8143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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