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 data is extracted from the following two-line orbital elements,
1 20355U 89090B 22092.41923698 0.00000000 00000-0 00000-0 0 01
2 20355 17.9037 355.9471 0289390 71.7823 291.3584 1.00725476 01
| Epoch (UTC): | 02 April 2022 10:03:42 |
| Eccentricity: | 0.0289390 |
| inclination: | 17.9037° |
| perigee height: | 34443 km |
| apogee height: | 36876 km |
| right ascension of ascending node: | 355.9471° |
| argument of perigee: | 71.7823° |
| revolutions per day: | 1.00725476 |
| mean anomaly at epoch: | 291.3584° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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