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 00016U 58002A 24280.36401333 .00000814 00000-0 11350-2 0 9996
2 00016 34.2649 294.6853 2024518 27.2793 342.0944 10.49439884623890
| Epoch (UTC): | 06 October 2024 08:44:10 |
| Eccentricity: | 0.2024518 |
| inclination: | 34.2649° |
| perigee height: | 650 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 294.6853° |
| argument of perigee: | 27.2793° |
| revolutions per day: | 10.49439884 |
| mean anomaly at epoch: | 342.0944° |
| orbit number at epoch: | 62389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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