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 19120U 88039B 22227.37446550 .00000079 00000-0 60611-4 0 9994
2 19120 71.0153 301.4488 0021981 183.3874 176.7105 14.19255277773855
| Epoch (UTC): | 15 August 2022 08:59:13 |
| Eccentricity: | 0.0021981 |
| inclination: | 71.0153° |
| perigee height: | 812 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 301.4488° |
| argument of perigee: | 183.3874° |
| revolutions per day: | 14.19255277 |
| mean anomaly at epoch: | 176.7105° |
| orbit number at epoch: | 77385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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