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 43012U 17072C 24340.49928046 .00001247 00000-0 25512-3 0 9994
2 43012 98.5877 59.7890 0125272 72.0745 289.4065 14.57884753375201
| Epoch (UTC): | 05 December 2024 11:58:57 |
| Eccentricity: | 0.0125272 |
| inclination: | 98.5877° |
| perigee height: | 611 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 59.7890° |
| argument of perigee: | 72.0745° |
| revolutions per day: | 14.57884753 |
| mean anomaly at epoch: | 289.4065° |
| orbit number at epoch: | 37520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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