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 20443U 26110.09084359 +.00000000 +00000-0 +58747-4 0 00009
2 20443 98.3007 169.5014 0011367 82.4767 277.7712 14.39896123 09
| Epoch (UTC): | 20 April 2026 02:10:48 |
| Eccentricity: | 0.0011367 |
| inclination: | 98.3007° |
| perigee height: | 751 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 169.5014° |
| argument of perigee: | 82.4767° |
| revolutions per day: | 14.39896123 |
| mean anomaly at epoch: | 277.7712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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