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 59790C 24093J 24281.09423611 -.00021286 00000+0 -50789-3 0 2817
2 59790 43.0024 274.1151 0001221 251.0048 77.2688 15.40719764 15
| Epoch (UTC): | 07 October 2024 02:15:42 |
| Eccentricity: | 0.0001221 |
| inclination: | 43.0024° |
| perigee height: | 443 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 274.1151° |
| argument of perigee: | 251.0048° |
| revolutions per day: | 15.40719764 |
| mean anomaly at epoch: | 77.2688° |
| 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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