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 21891U 26158.95386093 +.00000000 +00000-0 +20928-3 0 00003
2 21891 19.9944 211.5821 0037995 26.4151 333.8199 14.93800872 09
| Epoch (UTC): | 07 June 2026 22:53:33 |
| Eccentricity: | 0.0037995 |
| inclination: | 19.9944° |
| perigee height: | 560 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 211.5821° |
| argument of perigee: | 26.4151° |
| revolutions per day: | 14.93800872 |
| mean anomaly at epoch: | 333.8199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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