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 36582U 10021B 23150.92302869 .00000108 00000-0 00000-0 0 9997
2 36582 0.0428 286.0820 0002822 160.7950 146.7934 1.00277627 47791
| Epoch (UTC): | 30 May 2023 22:09:09 |
| Eccentricity: | 0.0002822 |
| inclination: | 0.0428° |
| perigee height: | 35772 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 286.0820° |
| argument of perigee: | 160.7950° |
| revolutions per day: | 1.00277627 |
| mean anomaly at epoch: | 146.7934° |
| orbit number at epoch: | 4779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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