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 25791U 26110.37134992 +.00000000 +00000-0 +53915-4 0 00002
2 25791 24.9856 2.6772 0010145 196.2155 163.8029 14.44450720 04
| Epoch (UTC): | 20 April 2026 08:54:44 |
| Eccentricity: | 0.0010145 |
| inclination: | 24.9856° |
| perigee height: | 737 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 2.6772° |
| argument of perigee: | 196.2155° |
| revolutions per day: | 14.44450720 |
| mean anomaly at epoch: | 163.8029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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