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 26100.13775009 +.00000000 +00000-0 +85124-4 0 00003
2 15595 108.0515 299.8178 0002040 254.5252 105.5665 14.39936166 08
| Epoch (UTC): | 10 April 2026 03:18:21 |
| Eccentricity: | 0.0002040 |
| inclination: | 108.0515° |
| perigee height: | 757 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 299.8178° |
| argument of perigee: | 254.5252° |
| revolutions per day: | 14.39936166 |
| mean anomaly at epoch: | 105.5665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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