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 43145U 18005A 24279.77248087 0.00000000 00000-0 00000-0 0 01
2 43145 106.0216 80.4036 0001815 130.4224 229.5776 13.47970721 06
| Epoch (UTC): | 05 October 2024 18:32:22 |
| Eccentricity: | 0.0001815 |
| inclination: | 106.0216° |
| perigee height: | 1078 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 80.4036° |
| argument of perigee: | 130.4224° |
| revolutions per day: | 13.47970721 |
| mean anomaly at epoch: | 229.5776° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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