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 23157.09628405 .00000033 00000-0 48325-4 0 9996
2 19468 99.1153 196.0870 0072362 124.8154 255.0317 14.03585644779088
| Epoch (UTC): | 06 June 2023 02:18:38 |
| Eccentricity: | 0.0072362 |
| inclination: | 99.1153° |
| perigee height: | 829 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 196.0870° |
| argument of perigee: | 124.8154° |
| revolutions per day: | 14.03585644 |
| mean anomaly at epoch: | 255.0317° |
| orbit number at epoch: | 77908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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