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 36110U 26145.40925073 +.00000000 +00000-0 +63391-4 0 00008
2 36110 98.0100 31.4140 0025896 111.4872 248.9103 14.77982599 06
| Epoch (UTC): | 25 May 2026 09:49:19 |
| Eccentricity: | 0.0025896 |
| inclination: | 98.0100° |
| perigee height: | 618 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 31.4140° |
| argument of perigee: | 111.4872° |
| revolutions per day: | 14.77982599 |
| mean anomaly at epoch: | 248.9103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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