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 19468U 88080B 23151.85145264 .00000341 00000-0 24028-3 0 9996
2 19468 99.1155 190.8289 0072166 139.3296 33.3983 14.03583030778134
| Epoch (UTC): | 31 May 2023 20:26:05 |
| Eccentricity: | 0.0072166 |
| inclination: | 99.1155° |
| perigee height: | 829 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 190.8289° |
| argument of perigee: | 139.3296° |
| revolutions per day: | 14.03583030 |
| mean anomaly at epoch: | 33.3983° |
| orbit number at epoch: | 77813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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