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 23331.65842509 .00011168 00000-0 74670-3 0 9998
2 43017 97.6044 209.6029 0222360 248.2356 109.5066 14.89080635325483
| Epoch (UTC): | 27 November 2023 15:48:07 |
| Eccentricity: | 0.0222360 |
| inclination: | 97.6044° |
| perigee height: | 445 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 209.6029° |
| argument of perigee: | 248.2356° |
| revolutions per day: | 14.89080635 |
| mean anomaly at epoch: | 109.5066° |
| orbit number at epoch: | 32548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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