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 42327U 95015JV 24356.01529330 .00008329 00000-0 30182-2 0 9999
2 42327 98.7091 19.1580 0005768 173.1945 186.9318 14.33624116475669
| Epoch (UTC): | 21 December 2024 00:22:01 |
| Eccentricity: | 0.0005768 |
| inclination: | 98.7091° |
| perigee height: | 775 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 19.1580° |
| argument of perigee: | 173.1945° |
| revolutions per day: | 14.33624116 |
| mean anomaly at epoch: | 186.9318° |
| orbit number at epoch: | 47566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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