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 29522U 06050A 21016.11884657 .00000004 00000-0 25041-4 0 9991
2 29522 98.7919 35.2089 0008903 294.8602 65.1645 14.14033098732780
| Epoch (UTC): | 16 January 2021 02:51:08 |
| Eccentricity: | 0.0008903 |
| inclination: | 98.7919° |
| perigee height: | 839 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 35.2089° |
| argument of perigee: | 294.8602° |
| revolutions per day: | 14.14033098 |
| mean anomaly at epoch: | 65.1645° |
| orbit number at epoch: | 73278 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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