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 26100.03150972 +.00000000 +00000-0 -12159-3 0 00008
2 25406 70.7381 62.4206 0004723 77.9679 282.1969 14.12453441 02
| Epoch (UTC): | 10 April 2026 00:45:22 |
| Eccentricity: | 0.0004723 |
| inclination: | 70.7381° |
| perigee height: | 848 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 62.4206° |
| argument of perigee: | 77.9679° |
| revolutions per day: | 14.12453441 |
| mean anomaly at epoch: | 282.1969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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