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 24298U 96051B 24281.82704384 .00000024 00000-0 39439-4 0 9997
2 24298 70.7924 190.7890 0015474 186.8037 173.2875 14.12455578448522
| Epoch (UTC): | 07 October 2024 19:50:56 |
| Eccentricity: | 0.0015474 |
| inclination: | 70.7924° |
| perigee height: | 840 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 190.7890° |
| argument of perigee: | 186.8037° |
| revolutions per day: | 14.12455578 |
| mean anomaly at epoch: | 173.2875° |
| orbit number at epoch: | 44852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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