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 23315.23943322 0.00015000 00000-0 22810-3 0 02
2 43941 73.5661 99.8223 0016807 338.1443 21.8556 15.54247637 03
| Epoch (UTC): | 11 November 2023 05:44:47 |
| Eccentricity: | 0.0016807 |
| inclination: | 73.5661° |
| perigee height: | 393 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 99.8223° |
| argument of perigee: | 338.1443° |
| revolutions per day: | 15.54247637 |
| mean anomaly at epoch: | 21.8556° |
| 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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