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 09023U 76069B 22146.35241375 .00000235 00000-0 83353-4 0 9993
2 09023 74.0442 6.5604 0016610 86.1081 274.1972 14.39768070404168
| Epoch (UTC): | 26 May 2022 08:27:28 |
| Eccentricity: | 0.0016610 |
| inclination: | 74.0442° |
| perigee height: | 747 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 6.5604° |
| argument of perigee: | 86.1081° |
| revolutions per day: | 14.39768070 |
| mean anomaly at epoch: | 274.1972° |
| orbit number at epoch: | 40416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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