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 21805U 26146.03007530 +.00000000 +00000-0 +00000-0 0 00006
2 21805 14.0146 345.6707 0004524 84.1068 278.2860 0.99184372 04
| Epoch (UTC): | 26 May 2026 00:43:18 |
| Eccentricity: | 0.0004524 |
| inclination: | 14.0146° |
| perigee height: | 36075 km |
| apogee height: | 36113 km |
| right ascension of ascending node: | 345.6707° |
| argument of perigee: | 84.1068° |
| revolutions per day: | 0.99184372 |
| mean anomaly at epoch: | 278.2860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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