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 26127.74881721 +.00000000 +00000-0 -40207-4 0 00006
2 22285 71.0224 240.2809 0006016 235.9373 124.1179 14.15461626 08
| Epoch (UTC): | 07 May 2026 17:58:17 |
| Eccentricity: | 0.0006016 |
| inclination: | 71.0224° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 240.2809° |
| argument of perigee: | 235.9373° |
| revolutions per day: | 14.15461626 |
| mean anomaly at epoch: | 124.1179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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