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 26161.96638539 +.00000000 +00000-0 +66862-4 0 00005
2 15595 108.0433 68.5029 0001285 284.0685 76.0314 14.39963425 02
| Epoch (UTC): | 10 June 2026 23:11:35 |
| Eccentricity: | 0.0001285 |
| inclination: | 108.0433° |
| perigee height: | 758 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 68.5029° |
| argument of perigee: | 284.0685° |
| revolutions per day: | 14.39963425 |
| mean anomaly at epoch: | 76.0314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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