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 22830U 26099.77298896 +.00000000 +00000-0 +88175-4 0 00003
2 22830 98.4863 168.0386 0010702 185.9130 174.1929 14.32878711 09
| Epoch (UTC): | 09 April 2026 18:33:06 |
| Eccentricity: | 0.0010702 |
| inclination: | 98.4863° |
| perigee height: | 774 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 168.0386° |
| argument of perigee: | 185.9130° |
| revolutions per day: | 14.32878711 |
| mean anomaly at epoch: | 174.1929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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