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 36230U 99025DVF 22341.01299992 .00001067 00000-0 10681-2 0 9994
2 36230 99.5705 44.6408 0230591 117.9626 244.5065 13.68918119467795
| Epoch (UTC): | 07 December 2022 00:18:43 |
| Eccentricity: | 0.0230591 |
| inclination: | 99.5705° |
| perigee height: | 833 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 44.6408° |
| argument of perigee: | 117.9626° |
| revolutions per day: | 13.68918119 |
| mean anomaly at epoch: | 244.5065° |
| orbit number at epoch: | 46779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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