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 19770U 89005B 24357.59275708 .00000478 00000-0 16045-3 0 9998
2 19770 74.0455 27.5900 0003893 162.6320 315.6204 14.39898325881186
| Epoch (UTC): | 22 December 2024 14:13:34 |
| Eccentricity: | 0.0003893 |
| inclination: | 74.0455° |
| perigee height: | 756 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 27.5900° |
| argument of perigee: | 162.6320° |
| revolutions per day: | 14.39898325 |
| mean anomaly at epoch: | 315.6204° |
| orbit number at epoch: | 88118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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