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 26063.35165282 +.00000000 +00000-0 +84261-4 0 00000
2 15593 82.5397 161.9744 0010114 325.7272 34.3291 14.86810417 08
| Epoch (UTC): | 04 March 2026 08:26:22 |
| Eccentricity: | 0.0010114 |
| inclination: | 82.5397° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 161.9744° |
| argument of perigee: | 325.7272° |
| revolutions per day: | 14.86810417 |
| mean anomaly at epoch: | 34.3291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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