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 25509U 26088.04133823 +.00000000 +00000-0 +86352-4 0 00000
2 25509 31.4291 211.5352 0336357 87.8174 276.0921 14.33288708 05
| Epoch (UTC): | 29 March 2026 00:59:31 |
| Eccentricity: | 0.0336357 |
| inclination: | 31.4291° |
| perigee height: | 540 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 211.5352° |
| argument of perigee: | 87.8174° |
| revolutions per day: | 14.33288708 |
| mean anomaly at epoch: | 276.0921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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