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 60800U 24140GB 24357.91156159 .00000370 00000-0 18758-3 0 9995
2 60800 89.0161 335.9910 0077574 137.6420 223.0791 14.12315278 18775
| Epoch (UTC): | 22 December 2024 21:52:38 |
| Eccentricity: | 0.0077574 |
| inclination: | 89.0161° |
| perigee height: | 795 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 335.9910° |
| argument of perigee: | 137.6420° |
| revolutions per day: | 14.12315278 |
| mean anomaly at epoch: | 223.0791° |
| orbit number at epoch: | 1877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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