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 22566U 93016B 24276.60775230 .00000133 00000-0 92760-4 0 9996
2 22566 71.0070 233.7118 0009065 26.4829 333.6755 14.15171439628165
| Epoch (UTC): | 02 October 2024 14:35:09 |
| Eccentricity: | 0.0009065 |
| inclination: | 71.0070° |
| perigee height: | 835 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 233.7118° |
| argument of perigee: | 26.4829° |
| revolutions per day: | 14.15171439 |
| mean anomaly at epoch: | 333.6755° |
| orbit number at epoch: | 62816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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