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 22826U 26145.12098986 +.00000000 +00000-0 +39953-4 0 00007
2 22826 98.6833 212.4568 0009608 145.5525 214.6283 14.31361097 08
| Epoch (UTC): | 25 May 2026 02:54:13 |
| Eccentricity: | 0.0009608 |
| inclination: | 98.6833° |
| perigee height: | 780 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 212.4568° |
| argument of perigee: | 145.5525° |
| revolutions per day: | 14.31361097 |
| mean anomaly at epoch: | 214.6283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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