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 43913U 18112E 24358.17364505 .00000544 00000-0 27910-3 0 9991
2 43913 50.0092 302.7611 0005154 267.8660 92.1665 14.28606795312023
| Epoch (UTC): | 23 December 2024 04:10:02 |
| Eccentricity: | 0.0005154 |
| inclination: | 50.0092° |
| perigee height: | 792 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 302.7611° |
| argument of perigee: | 267.8660° |
| revolutions per day: | 14.28606795 |
| mean anomaly at epoch: | 92.1665° |
| orbit number at epoch: | 31202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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