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 26106.57584662 +.00000000 +00000-0 +43653-4 0 00008
2 20442 98.8899 126.6712 0012112 31.8972 328.2942 14.34103489 04
| Epoch (UTC): | 16 April 2026 13:49:13 |
| Eccentricity: | 0.0012112 |
| inclination: | 98.8899° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 126.6712° |
| argument of perigee: | 31.8972° |
| revolutions per day: | 14.34103489 |
| mean anomaly at epoch: | 328.2942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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