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 25359U 98035B 23277.63033549 .00000248 00000-0 29903-3 0 9993
2 25359 26.3825 236.2840 0513648 41.4065 116.1915 12.94523141198716
| Epoch (UTC): | 04 October 2023 15:07:40 |
| Eccentricity: | 0.0513648 |
| inclination: | 26.3825° |
| perigee height: | 890 km |
| apogee height: | 1677 km |
| right ascension of ascending node: | 236.2840° |
| argument of perigee: | 41.4065° |
| revolutions per day: | 12.94523141 |
| mean anomaly at epoch: | 116.1915° |
| orbit number at epoch: | 19871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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