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 10793U 26064.25377539 +.00000000 +00000-0 +42320-3 0 00006
2 10793 28.2265 173.1781 0873958 170.6879 191.1058 13.07541881 06
| Epoch (UTC): | 05 March 2026 06:05:26 |
| Eccentricity: | 0.0873958 |
| inclination: | 28.2265° |
| perigee height: | 568 km |
| apogee height: | 1898 km |
| right ascension of ascending node: | 173.1781° |
| argument of perigee: | 170.6879° |
| revolutions per day: | 13.07541881 |
| mean anomaly at epoch: | 191.1058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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