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 43017U 17073E 23081.15734122 .00012210 00000-0 86887-3 0 9998
2 43017 97.6434 328.9499 0237912 356.8044 3.1638 14.84695715288265
| Epoch (UTC): | 22 March 2023 03:46:34 |
| Eccentricity: | 0.0237912 |
| inclination: | 97.6434° |
| perigee height: | 448 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 328.9499° |
| argument of perigee: | 356.8044° |
| revolutions per day: | 14.84695715 |
| mean anomaly at epoch: | 3.1638° |
| orbit number at epoch: | 28826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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