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 42320U 95015JN 24355.89380663 .00009247 00000-0 31369-2 0 9999
2 42320 98.6616 22.2123 0008037 66.3764 293.8265 14.36883585503915
| Epoch (UTC): | 20 December 2024 21:27:04 |
| Eccentricity: | 0.0008037 |
| inclination: | 98.6616° |
| perigee height: | 763 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 22.2123° |
| argument of perigee: | 66.3764° |
| revolutions per day: | 14.36883585 |
| mean anomaly at epoch: | 293.8265° |
| orbit number at epoch: | 50391 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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