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 26068.85800628 +.00000000 +00000-0 +19402-1 0 00004
2 59588 97.2069 9.9320 0059818 76.3572 284.4244 13.89619668 09
| Epoch (UTC): | 09 March 2026 20:35:31 |
| Eccentricity: | 0.0059818 |
| inclination: | 97.2069° |
| perigee height: | 886 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 9.9320° |
| argument of perigee: | 76.3572° |
| revolutions per day: | 13.89619668 |
| mean anomaly at epoch: | 284.4244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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