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 26064.92331187 +.00000000 +00000-0 -75538-4 0 00007
2 22285 71.0239 12.1715 0006354 297.6678 62.3799 14.15449013 01
| Epoch (UTC): | 05 March 2026 22:09:34 |
| Eccentricity: | 0.0006354 |
| inclination: | 71.0239° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 12.1715° |
| argument of perigee: | 297.6678° |
| revolutions per day: | 14.15449013 |
| mean anomaly at epoch: | 62.3799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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