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 21101.81930283 .00001046 00000-0 85609-4 0 9991
2 29507 97.7264 128.0596 0046476 240.2747 119.3847 15.00759122790117
| Epoch (UTC): | 11 April 2021 19:39:47 |
| Eccentricity: | 0.0046476 |
| inclination: | 97.7264° |
| perigee height: | 532 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 128.0596° |
| argument of perigee: | 240.2747° |
| revolutions per day: | 15.00759122 |
| mean anomaly at epoch: | 119.3847° |
| orbit number at epoch: | 79011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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