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 26109.12058919 +.00000000 +00000-0 +44487-4 0 00007
2 22826 98.6861 176.4573 0007782 254.9503 105.0819 14.31351209 08
| Epoch (UTC): | 19 April 2026 02:53:38 |
| Eccentricity: | 0.0007782 |
| inclination: | 98.6861° |
| perigee height: | 782 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 176.4573° |
| argument of perigee: | 254.9503° |
| revolutions per day: | 14.31351209 |
| mean anomaly at epoch: | 105.0819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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