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 26137.62050132 +.00000000 +00000-0 +57525-4 0 00004
2 22830 98.4830 205.1106 0011958 82.0111 278.2430 14.32893480 09
| Epoch (UTC): | 17 May 2026 14:53:31 |
| Eccentricity: | 0.0011958 |
| inclination: | 98.4830° |
| perigee height: | 774 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 205.1106° |
| argument of perigee: | 82.0111° |
| revolutions per day: | 14.32893480 |
| mean anomaly at epoch: | 278.2430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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