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 26106.95356780 +.00000000 +00000-0 +39814-4 0 00000
2 22826 98.6863 174.2898 0007745 262.2463 97.7841 14.31350696 03
| Epoch (UTC): | 16 April 2026 22:53:08 |
| Eccentricity: | 0.0007745 |
| inclination: | 98.6863° |
| perigee height: | 782 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 174.2898° |
| argument of perigee: | 262.2463° |
| revolutions per day: | 14.31350696 |
| mean anomaly at epoch: | 97.7841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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