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 26931U 26103.27235909 +.00000000 +00000-0 +66340-4 0 00006
2 26931 67.0513 52.1669 0006698 264.3866 95.6472 14.31930561 04
| Epoch (UTC): | 13 April 2026 06:32:11 |
| Eccentricity: | 0.0006698 |
| inclination: | 67.0513° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 52.1669° |
| argument of perigee: | 264.3866° |
| revolutions per day: | 14.31930561 |
| mean anomaly at epoch: | 95.6472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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