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 26065U 00004E 24358.14080145 .00000484 00000-0 17865-3 0 9994
2 26065 100.2265 186.9939 0036664 121.9879 238.4874 14.37868831305805
| Epoch (UTC): | 23 December 2024 03:22:45 |
| Eccentricity: | 0.0036664 |
| inclination: | 100.2265° |
| perigee height: | 739 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 186.9939° |
| argument of perigee: | 121.9879° |
| revolutions per day: | 14.37868831 |
| mean anomaly at epoch: | 238.4874° |
| orbit number at epoch: | 30580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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