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 is defined by the following mean orbital elements,
1 42478U 12008AN 24164.29735707 -.00000072 00000-0 00000+0 0 9992
2 42478 20.2787 114.2210 6806610 94.3229 339.6687 2.24186473 72974
| Epoch (UTC): | 12 June 2024 07:08:11 |
| Eccentricity: | 0.6806610 |
| inclination: | 20.2787° |
| perigee height: | 1497 km |
| apogee height: | 35067 km |
| right ascension of ascending node: | 114.2210° |
| argument of perigee: | 94.3229° |
| revolutions per day: | 2.24186473 |
| mean anomaly at epoch: | 339.6687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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