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 26160.32746646 +.00000000 +00000-0 -57735-4 0 00007
2 22285 71.0201 171.8914 0004389 199.9793 160.1159 14.15464555 07
| Epoch (UTC): | 09 June 2026 07:51:33 |
| Eccentricity: | 0.0004389 |
| inclination: | 71.0201° |
| perigee height: | 838 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 171.8914° |
| argument of perigee: | 199.9793° |
| revolutions per day: | 14.15464555 |
| mean anomaly at epoch: | 160.1159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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