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 13028U 82001B 23342.46251135 .00000219 00000-0 79462-4 0 9990
2 13028 74.0414 350.5431 0020249 211.4120 148.5827 14.38919370196966
| Epoch (UTC): | 08 December 2023 11:06:00 |
| Eccentricity: | 0.0020249 |
| inclination: | 74.0414° |
| perigee height: | 747 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 350.5431° |
| argument of perigee: | 211.4120° |
| revolutions per day: | 14.38919370 |
| mean anomaly at epoch: | 148.5827° |
| orbit number at epoch: | 19696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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