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 124U 61015J 24358.12339578 .00001098 00000-0 41093-3 0 9998
2 124 66.5433 240.1200 0068373 153.3591 207.1048 14.34251523281765
| Epoch (UTC): | 23 December 2024 02:57:41 |
| Eccentricity: | 0.0068373 |
| inclination: | 66.5433° |
| perigee height: | 728 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 240.1200° |
| argument of perigee: | 153.3591° |
| revolutions per day: | 14.34251523 |
| mean anomaly at epoch: | 207.1048° |
| orbit number at epoch: | 28176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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