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 20559U 26064.12599933 +.00000000 +00000-0 +98178-3 0 00009
2 20559 30.8041 250.1028 4112646 252.4058 59.5231 7.34005515 02
| Epoch (UTC): | 05 March 2026 03:01:26 |
| Eccentricity: | 0.4112646 |
| inclination: | 30.8041° |
| perigee height: | 206 km |
| apogee height: | 9406 km |
| right ascension of ascending node: | 250.1028° |
| argument of perigee: | 252.4058° |
| revolutions per day: | 7.34005515 |
| mean anomaly at epoch: | 59.5231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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