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 26087.41712929 +.00000000 +00000-0 +95030-4 0 00003
2 26931 67.0488 93.1758 0006897 264.7045 95.3270 14.31921117 03
| Epoch (UTC): | 28 March 2026 10:00:39 |
| Eccentricity: | 0.0006897 |
| inclination: | 67.0488° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 93.1758° |
| argument of perigee: | 264.7045° |
| revolutions per day: | 14.31921117 |
| mean anomaly at epoch: | 95.3270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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