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 21061.34682915 .00000815 00000-0 67695-4 0 9998
2 29507 97.7201 87.8455 0049104 17.3666 342.9223 15.00674880784097
| Epoch (UTC): | 02 March 2021 08:19:26 |
| Eccentricity: | 0.0049104 |
| inclination: | 97.7201° |
| perigee height: | 531 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 87.8455° |
| argument of perigee: | 17.3666° |
| revolutions per day: | 15.00674880 |
| mean anomaly at epoch: | 342.9223° |
| orbit number at epoch: | 78409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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