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 42425U 00055TV 24355.54530780 .00004513 00000-0 23392-2 0 9992
2 42425 98.7298 32.3020 0025153 326.1958 33.7611 14.15148604429721
| Epoch (UTC): | 20 December 2024 13:05:14 |
| Eccentricity: | 0.0025153 |
| inclination: | 98.7298° |
| perigee height: | 823 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 32.3020° |
| argument of perigee: | 326.1958° |
| revolutions per day: | 14.15148604 |
| mean anomaly at epoch: | 33.7611° |
| orbit number at epoch: | 42972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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