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 26091U 00004J 23270.51813243 .00003153 00000-0 79333-3 0 9993
2 26091 100.1909 148.4990 0028102 329.2400 30.7141 14.51912277245790
| Epoch (UTC): | 27 September 2023 12:26:06 |
| Eccentricity: | 0.0028102 |
| inclination: | 100.1909° |
| perigee height: | 699 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 148.4990° |
| argument of perigee: | 329.2400° |
| revolutions per day: | 14.51912277 |
| mean anomaly at epoch: | 30.7141° |
| orbit number at epoch: | 24579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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