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 43678U 18084H 23340.74297235 .00001662 00000-0 16063-3 0 9994
2 43678 98.0455 128.5550 0008490 316.8957 43.1597 14.94220769278029
| Epoch (UTC): | 06 December 2023 17:49:52 |
| Eccentricity: | 0.0008490 |
| inclination: | 98.0455° |
| perigee height: | 579 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 128.5550° |
| argument of perigee: | 316.8957° |
| revolutions per day: | 14.94220769 |
| mean anomaly at epoch: | 43.1597° |
| orbit number at epoch: | 27802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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