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 16U 58002A 24278.17399739 .00000830 00000-0 11535-2 0 9991
2 16 34.2653 301.0196 2024591 18.0328 348.2609 10.49436551623659
| Epoch (UTC): | 04 October 2024 04:10:33 |
| Eccentricity: | 0.2024591 |
| inclination: | 34.2653° |
| perigee height: | 650 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 301.0196° |
| argument of perigee: | 18.0328° |
| revolutions per day: | 10.49436551 |
| mean anomaly at epoch: | 348.2609° |
| orbit number at epoch: | 62365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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