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 20959U 26117.14881919 +.00000000 +00000-0 +00000-0 0 00006
2 20959 56.1597 53.4219 0022570 86.9848 273.2490 1.88155241 05
| Epoch (UTC): | 27 April 2026 03:34:17 |
| Eccentricity: | 0.0022570 |
| inclination: | 56.1597° |
| perigee height: | 21275 km |
| apogee height: | 21400 km |
| right ascension of ascending node: | 53.4219° |
| argument of perigee: | 86.9848° |
| revolutions per day: | 1.88155241 |
| mean anomaly at epoch: | 273.2490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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