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 26382U 26103.94724557 +.00000000 +00000-0 +00000-0 0 00009
2 26382 13.2099 17.3801 0003751 301.8307 235.3834 1.00098255 03
| Epoch (UTC): | 13 April 2026 22:44:02 |
| Eccentricity: | 0.0003751 |
| inclination: | 13.2099° |
| perigee height: | 35819 km |
| apogee height: | 35851 km |
| right ascension of ascending node: | 17.3801° |
| argument of perigee: | 301.8307° |
| revolutions per day: | 1.00098255 |
| mean anomaly at epoch: | 235.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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