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 26160.10532169 +.00000000 +00000-0 +74664-4 0 00001
2 22830 98.4819 227.1301 0010978 20.2194 339.9423 14.32904458 08
| Epoch (UTC): | 09 June 2026 02:31:39 |
| Eccentricity: | 0.0010978 |
| inclination: | 98.4819° |
| perigee height: | 774 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 227.1301° |
| argument of perigee: | 20.2194° |
| revolutions per day: | 14.32904458 |
| mean anomaly at epoch: | 339.9423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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