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 24926U 97048B 24358.15776133 .00000786 00000-0 85789-4 0 9998
2 24926 86.3354 218.2170 0009708 68.4077 291.8181 14.86443893478998
| Epoch (UTC): | 23 December 2024 03:47:10 |
| Eccentricity: | 0.0009708 |
| inclination: | 86.3354° |
| perigee height: | 602 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 218.2170° |
| argument of perigee: | 68.4077° |
| revolutions per day: | 14.86443893 |
| mean anomaly at epoch: | 291.8181° |
| orbit number at epoch: | 47899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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