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 26052U 00001A 23273.10263840 .00000030 00000-0 00000+0 0 9999
2 26052 10.2865 39.4661 0002861 188.6338 357.6939 1.00271674 21689
| Epoch (UTC): | 30 September 2023 02:27:47 |
| Eccentricity: | 0.0002861 |
| inclination: | 10.2865° |
| perigee height: | 35774 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 39.4661° |
| argument of perigee: | 188.6338° |
| revolutions per day: | 1.00271674 |
| mean anomaly at epoch: | 357.6939° |
| orbit number at epoch: | 2168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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