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 22285U 26073.47440271 +.00000000 +00000-0 -34702-5 0 00001
2 22285 71.0241 354.2224 0006317 288.8537 71.1901 14.15447032 06
| Epoch (UTC): | 14 March 2026 11:23:08 |
| Eccentricity: | 0.0006317 |
| inclination: | 71.0241° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 354.2224° |
| argument of perigee: | 288.8537° |
| revolutions per day: | 14.15447032 |
| mean anomaly at epoch: | 71.1901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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