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 20323U 26088.14086725 +.00000000 +00000-0 +98905-4 0 00005
2 20323 97.0692 292.4834 0070491 61.7406 299.0884 14.50678751 06
| Epoch (UTC): | 29 March 2026 03:22:50 |
| Eccentricity: | 0.0070491 |
| inclination: | 97.0692° |
| perigee height: | 673 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 292.4834° |
| argument of perigee: | 61.7406° |
| revolutions per day: | 14.50678751 |
| mean anomaly at epoch: | 299.0884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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