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 43937U 19003F 23276.03552623 .00236764 00000-0 15965-2 0 9991
2 43937 97.0703 303.1504 0007085 206.7047 153.3855 15.74399168262874
| Epoch (UTC): | 03 October 2023 00:51:09 |
| Eccentricity: | 0.0007085 |
| inclination: | 97.0703° |
| perigee height: | 341 km |
| apogee height: | 351 km |
| right ascension of ascending node: | 303.1504° |
| argument of perigee: | 206.7047° |
| revolutions per day: | 15.74399168 |
| mean anomaly at epoch: | 153.3855° |
| orbit number at epoch: | 26287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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