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 23081.61381690 .00002859 00000-0 28013-3 0 9998
2 43678 98.0050 223.9299 0010771 88.8670 271.3795 14.93048550239345
| Epoch (UTC): | 22 March 2023 14:43:53 |
| Eccentricity: | 0.0010771 |
| inclination: | 98.0050° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 223.9299° |
| argument of perigee: | 88.8670° |
| revolutions per day: | 14.93048550 |
| mean anomaly at epoch: | 271.3795° |
| orbit number at epoch: | 23934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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