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 06236U 72082B 23342.54019677 -.00000025 00000-0 13742-3 0 9997
2 06236 102.0158 339.4649 0004456 104.3243 9.5051 12.53182561339515
| Epoch (UTC): | 08 December 2023 12:57:53 |
| Eccentricity: | 0.0004456 |
| inclination: | 102.0158° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 339.4649° |
| argument of perigee: | 104.3243° |
| revolutions per day: | 12.53182561 |
| mean anomaly at epoch: | 9.5051° |
| orbit number at epoch: | 33951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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