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 29507U 06046C 21027.07366819 .00000467 00000-0 40997-4 0 9991
2 29507 97.7173 53.8198 0047423 129.5222 231.0209 15.00628751778954
| Epoch (UTC): | 27 January 2021 01:46:04 |
| Eccentricity: | 0.0047423 |
| inclination: | 97.7173° |
| perigee height: | 532 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 53.8198° |
| argument of perigee: | 129.5222° |
| revolutions per day: | 15.00628751 |
| mean anomaly at epoch: | 231.0209° |
| orbit number at epoch: | 77895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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