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 24357.90570790 .00017278 00000-0 95214-3 0 9990
2 43017 97.5474 227.1733 0191526 19.8513 341.0033 14.99674721383883
| Epoch (UTC): | 22 December 2024 21:44:13 |
| Eccentricity: | 0.0191526 |
| inclination: | 97.5474° |
| perigee height: | 435 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 227.1733° |
| argument of perigee: | 19.8513° |
| revolutions per day: | 14.99674721 |
| mean anomaly at epoch: | 341.0033° |
| orbit number at epoch: | 38388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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