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 22220U 92076B 24281.82507369 .00000607 00000-0 32722-3 0 9991
2 22220 71.0008 199.1432 0012444 174.6755 241.6156 14.16711925648814
| Epoch (UTC): | 07 October 2024 19:48:06 |
| Eccentricity: | 0.0012444 |
| inclination: | 71.0008° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 199.1432° |
| argument of perigee: | 174.6755° |
| revolutions per day: | 14.16711925 |
| mean anomaly at epoch: | 241.6156° |
| orbit number at epoch: | 64881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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