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 20480U 26110.56075706 +.00000000 +00000-0 +36913-6 0 00001
2 20480 99.0708 44.1591 0539122 275.1225 78.8587 12.83488855 04
| Epoch (UTC): | 20 April 2026 13:27:29 |
| Eccentricity: | 0.0539122 |
| inclination: | 99.0708° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 44.1591° |
| argument of perigee: | 275.1225° |
| revolutions per day: | 12.83488855 |
| mean anomaly at epoch: | 78.8587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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