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 23090.63753823 .00063929 00000-0 13583-2 0 9991
2 43937 97.0983 119.2107 0015341 190.4045 169.6889 15.44665502234040
| Epoch (UTC): | 31 March 2023 15:18:03 |
| Eccentricity: | 0.0015341 |
| inclination: | 97.0983° |
| perigee height: | 422 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 119.2107° |
| argument of perigee: | 190.4045° |
| revolutions per day: | 15.44665502 |
| mean anomaly at epoch: | 169.6889° |
| orbit number at epoch: | 23404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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