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 20442U 26110.62247684 +.00000000 +00000-0 +40848-4 0 00002
2 20442 98.8895 130.8313 0011903 20.5114 339.6546 14.34104439 06
| Epoch (UTC): | 20 April 2026 14:56:21 |
| Eccentricity: | 0.0011903 |
| inclination: | 98.8895° |
| perigee height: | 770 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 130.8313° |
| argument of perigee: | 20.5114° |
| revolutions per day: | 14.34104439 |
| mean anomaly at epoch: | 339.6546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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