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 19223U 88052A 23083.26470713 .00000172 00000-0 38871-3 0 9996
2 19223 89.9721 80.1740 0029087 232.2496 138.5505 13.22776948678275
| Epoch (UTC): | 24 March 2023 06:21:10 |
| Eccentricity: | 0.0029087 |
| inclination: | 89.9721° |
| perigee height: | 1152 km |
| apogee height: | 1196 km |
| right ascension of ascending node: | 80.1740° |
| argument of perigee: | 232.2496° |
| revolutions per day: | 13.22776948 |
| mean anomaly at epoch: | 138.5505° |
| orbit number at epoch: | 67827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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