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 26073.39957985 +.00000000 +00000-0 +68226-4 0 00004
2 22826 98.6921 140.7210 0008927 9.6918 350.4436 14.31338983 09
| Epoch (UTC): | 14 March 2026 09:35:23 |
| Eccentricity: | 0.0008927 |
| inclination: | 98.6921° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 140.7210° |
| argument of perigee: | 9.6918° |
| revolutions per day: | 14.31338983 |
| mean anomaly at epoch: | 350.4436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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