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 01360U 65034B 24256.60926456 -.00000023 00000-0 00000-0 0 9991
2 01360 32.2054 33.2121 3967308 206.7941 125.6898 4.64829702 7980
| Epoch (UTC): | 12 September 2024 14:37:20 |
| Eccentricity: | 0.3967308 |
| inclination: | 32.2054° |
| perigee height: | 2771 km |
| apogee height: | 14804 km |
| right ascension of ascending node: | 33.2121° |
| argument of perigee: | 206.7941° |
| revolutions per day: | 4.64829702 |
| mean anomaly at epoch: | 125.6898° |
| orbit number at epoch: | 798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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