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 24262.58940408 .00017825 00000-0 10483-2 0 9998
2 43017 97.5610 134.8480 0201495 341.4146 17.9788 14.96171026369619
| Epoch (UTC): | 18 September 2024 14:08:44 |
| Eccentricity: | 0.0201495 |
| inclination: | 97.5610° |
| perigee height: | 438 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 134.8480° |
| argument of perigee: | 341.4146° |
| revolutions per day: | 14.96171026 |
| mean anomaly at epoch: | 17.9788° |
| orbit number at epoch: | 36961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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