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 22638U 26088.16059065 +.00000000 +00000-0 +70635-4 0 00005
2 22638 69.9190 119.3130 0062265 267.9650 91.4344 14.33644673 07
| Epoch (UTC): | 29 March 2026 03:51:15 |
| Eccentricity: | 0.0062265 |
| inclination: | 69.9190° |
| perigee height: | 735 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 119.3130° |
| argument of perigee: | 267.9650° |
| revolutions per day: | 14.33644673 |
| mean anomaly at epoch: | 91.4344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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