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 15595U 26053.66109623 +.00000000 +00000-0 +11432-3 0 00001
2 15595 108.0460 203.0693 0002533 264.6371 95.4482 14.39899302 01
| Epoch (UTC): | 22 February 2026 15:51:58 |
| Eccentricity: | 0.0002533 |
| inclination: | 108.0460° |
| perigee height: | 757 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 203.0693° |
| argument of perigee: | 264.6371° |
| revolutions per day: | 14.39899302 |
| mean anomaly at epoch: | 95.4482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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