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 26162.20017068 +.00000000 +00000-0 +68535-4 0 00000
2 22830 98.4818 229.1814 0010849 14.1387 346.0099 14.32905321 09
| Epoch (UTC): | 11 June 2026 04:48:14 |
| Eccentricity: | 0.0010849 |
| inclination: | 98.4818° |
| perigee height: | 774 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 229.1814° |
| argument of perigee: | 14.1387° |
| revolutions per day: | 14.32905321 |
| mean anomaly at epoch: | 346.0099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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