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 36133U 09075C 23265.45033000 .00001001 00000-0 10253-2 0 9995
2 36133 45.8926 322.5955 5141421 200.8887 126.7059 5.22649203260601
| Epoch (UTC): | 22 September 2023 10:48:28 |
| Eccentricity: | 0.5141421 |
| inclination: | 45.8926° |
| perigee height: | 436 km |
| apogee height: | 14859 km |
| right ascension of ascending node: | 322.5955° |
| argument of perigee: | 200.8887° |
| revolutions per day: | 5.22649203 |
| mean anomaly at epoch: | 126.7059° |
| orbit number at epoch: | 26060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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