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 59793C 24093M 24252.09284722 .00103240 00000+0 22082-2 0 2527
2 59793 43.0028 80.9331 0004577 304.8978 5.0113 15.43841663 10
| Epoch (UTC): | 08 September 2024 02:13:42 |
| Eccentricity: | 0.0004577 |
| inclination: | 43.0028° |
| perigee height: | 431 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 80.9331° |
| argument of perigee: | 304.8978° |
| revolutions per day: | 15.43841663 |
| mean anomaly at epoch: | 5.0113° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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