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 26017.71554034 +.00000000 +00000-0 +17812-3 0 00009
2 22285 71.0223 111.2774 0003908 353.2719 6.8351 14.15438706 01
| Epoch (UTC): | 17 January 2026 17:10:22 |
| Eccentricity: | 0.0003908 |
| inclination: | 71.0223° |
| perigee height: | 838 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 111.2774° |
| argument of perigee: | 353.2719° |
| revolutions per day: | 14.15438706 |
| mean anomaly at epoch: | 6.8351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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