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 11574U 79089B 23338.55101222 .00000501 00000-0 16273-3 0 9996
2 11574 74.0677 179.1116 0016267 205.4373 154.5984 14.41333832317237
| Epoch (UTC): | 04 December 2023 13:13:27 |
| Eccentricity: | 0.0016267 |
| inclination: | 74.0677° |
| perigee height: | 742 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 179.1116° |
| argument of perigee: | 205.4373° |
| revolutions per day: | 14.41333832 |
| mean anomaly at epoch: | 154.5984° |
| orbit number at epoch: | 31723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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