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 260U 61015CG 24357.94579360 .00003875 00000-0 12134-2 0 9991
2 260 66.7676 202.8765 0045631 173.3251 186.8472 14.41064186278726
| Epoch (UTC): | 22 December 2024 22:41:56 |
| Eccentricity: | 0.0045631 |
| inclination: | 66.7676° |
| perigee height: | 722 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 202.8765° |
| argument of perigee: | 173.3251° |
| revolutions per day: | 14.41064186 |
| mean anomaly at epoch: | 186.8472° |
| orbit number at epoch: | 27872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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