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 26071.76408769 +.00000000 +00000-0 +63270-4 0 00001
2 15593 82.5395 154.0744 0009685 294.2677 65.7528 14.86820691 05
| Epoch (UTC): | 12 March 2026 18:20:17 |
| Eccentricity: | 0.0009685 |
| inclination: | 82.5395° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 154.0744° |
| argument of perigee: | 294.2677° |
| revolutions per day: | 14.86820691 |
| mean anomaly at epoch: | 65.7528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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