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 22180.45273388 .00000394 00000-0 44459-4 0 9998
2 43678 97.9720 313.8592 0008597 242.5549 117.4809 14.92186330199641
| Epoch (UTC): | 29 June 2022 10:51:56 |
| Eccentricity: | 0.0008597 |
| inclination: | 97.9720° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 313.8592° |
| argument of perigee: | 242.5549° |
| revolutions per day: | 14.92186330 |
| mean anomaly at epoch: | 117.4809° |
| orbit number at epoch: | 19964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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