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 26280U 26088.08253647 +.00000000 +00000-0 +13571-3 0 00000
2 26280 98.7321 137.0562 0085885 68.6797 320.8715 14.38410746 05
| Epoch (UTC): | 29 March 2026 01:58:51 |
| Eccentricity: | 0.0085885 |
| inclination: | 98.7321° |
| perigee height: | 702 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 137.0562° |
| argument of perigee: | 68.6797° |
| revolutions per day: | 14.38410746 |
| mean anomaly at epoch: | 320.8715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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