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 26356U 00024A 23081.25523834 .00000084 00000-0 00000+0 0 9995
2 26356 12.2850 19.7167 0001515 223.7056 222.1962 1.00267645 19746
| Epoch (UTC): | 22 March 2023 06:07:32 |
| Eccentricity: | 0.0001515 |
| inclination: | 12.2850° |
| perigee height: | 35781 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 19.7167° |
| argument of perigee: | 223.7056° |
| revolutions per day: | 1.00267645 |
| mean anomaly at epoch: | 222.1962° |
| orbit number at epoch: | 1974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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