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 25406U 26069.57937525 +.00000000 +00000-0 -11557-3 0 00009
2 25406 70.7414 126.9469 0004303 143.2410 216.9005 14.12467111 05
| Epoch (UTC): | 10 March 2026 13:54:18 |
| Eccentricity: | 0.0004303 |
| inclination: | 70.7414° |
| perigee height: | 848 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 126.9469° |
| argument of perigee: | 143.2410° |
| revolutions per day: | 14.12467111 |
| mean anomaly at epoch: | 216.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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