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 22179.78216456 .00000313 00000-0 36496-4 0 9998
2 43678 97.9719 313.1808 0008554 244.9707 115.0633 14.92185043199545
| Epoch (UTC): | 28 June 2022 18:46:19 |
| Eccentricity: | 0.0008554 |
| inclination: | 97.9719° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 313.1808° |
| argument of perigee: | 244.9707° |
| revolutions per day: | 14.92185043 |
| mean anomaly at epoch: | 115.0633° |
| orbit number at epoch: | 19954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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