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 36799U 10035E 24259.64477545 .00023244 00000-0 16225-2 0 9990
2 36799 98.0766 153.1004 0001934 309.7242 50.3813 15.05362923770651
| Epoch (UTC): | 15 September 2024 15:28:28 |
| Eccentricity: | 0.0001934 |
| inclination: | 98.0766° |
| perigee height: | 549 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 153.1004° |
| argument of perigee: | 309.7242° |
| revolutions per day: | 15.05362923 |
| mean anomaly at epoch: | 50.3813° |
| orbit number at epoch: | 77065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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