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 14401U 83103A 23340.48928604 .00000205 00000-0 85202-4 0 9996
2 14401 74.0449 359.9016 0013714 341.9986 18.0678 14.32539345 97183
| Epoch (UTC): | 06 December 2023 11:44:34 |
| Eccentricity: | 0.0013714 |
| inclination: | 74.0449° |
| perigee height: | 773 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 359.9016° |
| argument of perigee: | 341.9986° |
| revolutions per day: | 14.32539345 |
| mean anomaly at epoch: | 18.0678° |
| orbit number at epoch: | 9718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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