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 26138.20791568 +.00000000 +00000-0 -44527-4 0 00007
2 22285 71.0214 218.3257 0005564 223.0086 137.0603 14.15458073 03
| Epoch (UTC): | 18 May 2026 04:59:23 |
| Eccentricity: | 0.0005564 |
| inclination: | 71.0214° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 218.3257° |
| argument of perigee: | 223.0086° |
| revolutions per day: | 14.15458073 |
| mean anomaly at epoch: | 137.0603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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