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 26106.80695928 +.00000000 +00000-0 +56491-4 0 00009
2 15595 108.0509 313.7016 0001919 253.3908 106.7024 14.39938506 09
| Epoch (UTC): | 16 April 2026 19:22:01 |
| Eccentricity: | 0.0001919 |
| inclination: | 108.0509° |
| perigee height: | 757 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 313.7016° |
| argument of perigee: | 253.3908° |
| revolutions per day: | 14.39938506 |
| mean anomaly at epoch: | 106.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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