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 25758U 26113.92706227 +.00000000 +00000-0 +75962-4 0 00001
2 25758 97.9660 89.3755 0002304 350.6571 9.4584 14.55232735 06
| Epoch (UTC): | 23 April 2026 22:14:58 |
| Eccentricity: | 0.0002304 |
| inclination: | 97.9660° |
| perigee height: | 707 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 89.3755° |
| argument of perigee: | 350.6571° |
| revolutions per day: | 14.55232735 |
| mean anomaly at epoch: | 9.4584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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