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 10521U 26100.01099404 +.00000000 +00000-0 +83945-4 0 00001
2 10521 74.0259 65.3660 0019913 9.9491 350.2055 14.42412627 02
| Epoch (UTC): | 10 April 2026 00:15:49 |
| Eccentricity: | 0.0019913 |
| inclination: | 74.0259° |
| perigee height: | 736 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 65.3660° |
| argument of perigee: | 9.9491° |
| revolutions per day: | 14.42412627 |
| mean anomaly at epoch: | 350.2055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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