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 26069.76454889 +.00000000 +00000-0 +71019-4 0 00009
2 22826 98.6927 137.0831 0009130 20.1220 340.0321 14.31337572 05
| Epoch (UTC): | 10 March 2026 18:20:57 |
| Eccentricity: | 0.0009130 |
| inclination: | 98.6927° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 137.0831° |
| argument of perigee: | 20.1220° |
| revolutions per day: | 14.31337572 |
| mean anomaly at epoch: | 340.0321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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