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 23129.91603666 0.00011500 00000-0 17975-3 0 01
2 43941 73.6781 160.1942 0022443 98.3370 261.6629 15.53358937 04
| Epoch (UTC): | 09 May 2023 21:59:05 |
| Eccentricity: | 0.0022443 |
| inclination: | 73.6781° |
| perigee height: | 392 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 160.1942° |
| argument of perigee: | 98.3370° |
| revolutions per day: | 15.53358937 |
| mean anomaly at epoch: | 261.6629° |
| 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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