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 24279U 96046C 24277.93202316 .00000371 00000-0 50992-3 0 9996
2 24279 98.6928 283.5116 0299118 330.1606 86.0311 13.47344893382900
| Epoch (UTC): | 03 October 2024 22:22:06 |
| Eccentricity: | 0.0299118 |
| inclination: | 98.6928° |
| perigee height: | 859 km |
| apogee height: | 1305 km |
| right ascension of ascending node: | 283.5116° |
| argument of perigee: | 330.1606° |
| revolutions per day: | 13.47344893 |
| mean anomaly at epoch: | 86.0311° |
| orbit number at epoch: | 38290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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