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 22224.69619769 .00000139 00000-0 89086-4 0 9994
2 19120 71.0156 307.1083 0022144 187.3726 172.7076 14.19254488773209
| Epoch (UTC): | 12 August 2022 16:42:31 |
| Eccentricity: | 0.0022144 |
| inclination: | 71.0156° |
| perigee height: | 812 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 307.1083° |
| argument of perigee: | 187.3726° |
| revolutions per day: | 14.19254488 |
| mean anomaly at epoch: | 172.7076° |
| orbit number at epoch: | 77320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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