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 26075.14718976 +.00000000 +00000-0 +66920-4 0 00003
2 22826 98.6916 142.4698 0008831 4.5801 355.5461 14.31339594 04
| Epoch (UTC): | 16 March 2026 03:31:57 |
| Eccentricity: | 0.0008831 |
| inclination: | 98.6916° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 142.4698° |
| argument of perigee: | 4.5801° |
| revolutions per day: | 14.31339594 |
| mean anomaly at epoch: | 355.5461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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