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 26073.31196999 +.00000000 +00000-0 +55383-4 0 00009
2 15593 82.5392 152.6205 0009611 288.3867 71.6305 14.86822197 04
| Epoch (UTC): | 14 March 2026 07:29:14 |
| Eccentricity: | 0.0009611 |
| inclination: | 82.5392° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 152.6205° |
| argument of perigee: | 288.3867° |
| revolutions per day: | 14.86822197 |
| mean anomaly at epoch: | 71.6305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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