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 31598U 26066.19054748 +.00000000 +00000-0 +35570-3 0 00000
2 31598 97.8866 257.2026 0000992 100.1471 259.9861 14.96508951 08
| Epoch (UTC): | 07 March 2026 04:34:23 |
| Eccentricity: | 0.0000992 |
| inclination: | 97.8866° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 257.2026° |
| argument of perigee: | 100.1471° |
| revolutions per day: | 14.96508951 |
| mean anomaly at epoch: | 259.9861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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