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 23089.53620003 .00063221 00000-0 13500-2 0 9995
2 43937 97.0986 118.1349 0015211 194.1440 165.9385 15.44523097233877
| Epoch (UTC): | 30 March 2023 12:52:07 |
| Eccentricity: | 0.0015211 |
| inclination: | 97.0986° |
| perigee height: | 422 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 118.1349° |
| argument of perigee: | 194.1440° |
| revolutions per day: | 15.44523097 |
| mean anomaly at epoch: | 165.9385° |
| orbit number at epoch: | 23387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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