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 23079.03659850 .00045222 00000-0 10080-2 0 9992
2 43937 97.1000 107.8852 0013957 234.5446 125.4500 15.43352191232254
| Epoch (UTC): | 20 March 2023 00:52:42 |
| Eccentricity: | 0.0013957 |
| inclination: | 97.1000° |
| perigee height: | 427 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 107.8852° |
| argument of perigee: | 234.5446° |
| revolutions per day: | 15.43352191 |
| mean anomaly at epoch: | 125.4500° |
| orbit number at epoch: | 23225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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