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 36255U 99025DWG 24352.44795436 .00003520 00000-0 12412-2 0 9996
2 36255 99.4529 233.4592 0066598 124.2073 49.0604 14.34239055588417
| Epoch (UTC): | 17 December 2024 10:45:03 |
| Eccentricity: | 0.0066598 |
| inclination: | 99.4529° |
| perigee height: | 730 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 233.4592° |
| argument of perigee: | 124.2073° |
| revolutions per day: | 14.34239055 |
| mean anomaly at epoch: | 49.0604° |
| orbit number at epoch: | 58841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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