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 02422U 26088.17452647 +.00000000 +00000-0 +16044-3 0 00001
2 02422 98.2325 245.0814 0111361 91.2866 270.1087 14.46712057 02
| Epoch (UTC): | 29 March 2026 04:11:19 |
| Eccentricity: | 0.0111361 |
| inclination: | 98.2325° |
| perigee height: | 657 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 245.0814° |
| argument of perigee: | 91.2866° |
| revolutions per day: | 14.46712057 |
| mean anomaly at epoch: | 270.1087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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