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 is defined by the following mean orbital elements,
1 26463U 00045A 25293.57799104 .00003729 00000-0 00000-0 0 9994
2 26463 145.9975 98.1036 9083513 317.9304 1.7530 0.45057109 19104
| Epoch (UTC): | 20 October 2025 13:52:18 |
| Eccentricity: | 0.9083513 |
| inclination: | 145.9975° |
| perigee height: | 209 km |
| apogee height: | 130777 km |
| right ascension of ascending node: | 98.1036° |
| argument of perigee: | 317.9304° |
| revolutions per day: | 0.45057109 |
| mean anomaly at epoch: | 1.7530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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