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 43941U 19004A 24257.78042836 0.00031000 00000-0 46859-3 0 05
2 43941 73.5710 122.9763 0020526 336.2450 23.7549 15.54327542 02
| Epoch (UTC): | 13 September 2024 18:43:49 |
| Eccentricity: | 0.0020526 |
| inclination: | 73.5710° |
| perigee height: | 390 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 122.9763° |
| argument of perigee: | 336.2450° |
| revolutions per day: | 15.54327542 |
| mean anomaly at epoch: | 23.7549° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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