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 26088.20471740 +.00000000 +00000-0 -11403-3 0 00002
2 25406 70.7378 87.4819 0004327 102.2218 257.9387 14.12458391 09
| Epoch (UTC): | 29 March 2026 04:54:47 |
| Eccentricity: | 0.0004327 |
| inclination: | 70.7378° |
| perigee height: | 848 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 87.4819° |
| argument of perigee: | 102.2218° |
| revolutions per day: | 14.12458391 |
| mean anomaly at epoch: | 257.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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