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 26068.48851029 +.00000000 +00000-0 +11227-3 0 00009
2 26931 67.0507 142.1332 0007015 265.3521 94.6779 14.31912188 01
| Epoch (UTC): | 09 March 2026 11:43:27 |
| Eccentricity: | 0.0007015 |
| inclination: | 67.0507° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 142.1332° |
| argument of perigee: | 265.3521° |
| revolutions per day: | 14.31912188 |
| mean anomaly at epoch: | 94.6779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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