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 26066.45811475 +.00000000 +00000-0 +96084-4 0 00001
2 20442 98.8937 85.4217 0012258 140.5591 219.6487 14.34087081 01
| Epoch (UTC): | 07 March 2026 10:59:41 |
| Eccentricity: | 0.0012258 |
| inclination: | 98.8937° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 85.4217° |
| argument of perigee: | 140.5591° |
| revolutions per day: | 14.34087081 |
| mean anomaly at epoch: | 219.6487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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