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 29777U 99025BT 22176.83309294 .00000106 00000-0 11647-3 0 9992
2 29777 99.4505 204.8118 0094049 20.9751 154.6576 13.91427751784328
| Epoch (UTC): | 25 June 2022 19:59:39 |
| Eccentricity: | 0.0094049 |
| inclination: | 99.4505° |
| perigee height: | 855 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 204.8118° |
| argument of perigee: | 20.9751° |
| revolutions per day: | 13.91427751 |
| mean anomaly at epoch: | 154.6576° |
| orbit number at epoch: | 78432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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