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 15593U 26064.69764656 +.00000000 +00000-0 +79909-4 0 00001
2 15593 82.5397 160.7104 0010029 320.7497 39.2992 14.86811927 03
| Epoch (UTC): | 05 March 2026 16:44:36 |
| Eccentricity: | 0.0010029 |
| inclination: | 82.5397° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 160.7104° |
| argument of perigee: | 320.7497° |
| revolutions per day: | 14.86811927 |
| mean anomaly at epoch: | 39.2992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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