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 07274U 74025A 24357.79456272 .00000090 00000-0 45028-4 0 9993
2 07274 81.2104 105.1058 0019177 64.6818 295.6336 14.08748326602078
| Epoch (UTC): | 22 December 2024 19:04:10 |
| Eccentricity: | 0.0019177 |
| inclination: | 81.2104° |
| perigee height: | 850 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 105.1058° |
| argument of perigee: | 64.6818° |
| revolutions per day: | 14.08748326 |
| mean anomaly at epoch: | 295.6336° |
| orbit number at epoch: | 60207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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