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 59588U 26097.06962785 +.00000000 +00000-0 +15764-1 0 00009
2 59588 97.1934 31.8050 0073145 13.3649 346.9431 13.91079864 01
| Epoch (UTC): | 07 April 2026 01:40:15 |
| Eccentricity: | 0.0073145 |
| inclination: | 97.1934° |
| perigee height: | 871 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 31.8050° |
| argument of perigee: | 13.3649° |
| revolutions per day: | 13.91079864 |
| mean anomaly at epoch: | 346.9431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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