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 22490U 26106.07301708 +.00000000 +00000-0 +45075-4 0 00006
2 22490 24.9687 231.0866 0041790 200.3716 315.4709 14.46092134 04
| Epoch (UTC): | 16 April 2026 01:45:08 |
| Eccentricity: | 0.0041790 |
| inclination: | 24.9687° |
| perigee height: | 709 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 231.0866° |
| argument of perigee: | 200.3716° |
| revolutions per day: | 14.46092134 |
| mean anomaly at epoch: | 315.4709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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