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 22177.43516606 .00000421 00000-0 47092-4 0 9992
2 43678 97.9716 310.8059 0008525 253.3601 106.6670 14.92183879199192
| Epoch (UTC): | 26 June 2022 10:26:38 |
| Eccentricity: | 0.0008525 |
| inclination: | 97.9716° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 310.8059° |
| argument of perigee: | 253.3601° |
| revolutions per day: | 14.92183879 |
| mean anomaly at epoch: | 106.6670° |
| orbit number at epoch: | 19919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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