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 20355U 26140.23881963 +.00000000 +00000-0 +00000-0 0 00001
2 20355 16.9082 341.0500 0291081 114.3323 242.4437 1.00731509 06
| Epoch (UTC): | 20 May 2026 05:43:54 |
| Eccentricity: | 0.0291081 |
| inclination: | 16.9082° |
| perigee height: | 34435 km |
| apogee height: | 36882 km |
| right ascension of ascending node: | 341.0500° |
| argument of perigee: | 114.3323° |
| revolutions per day: | 1.00731509 |
| mean anomaly at epoch: | 242.4437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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