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 23028.47071821 .00000373 00000-0 12387-3 0 9993
2 11574 74.0694 31.9758 0014882 137.8871 222.3431 14.41019549272366
| Epoch (UTC): | 28 January 2023 11:17:50 |
| Eccentricity: | 0.0014882 |
| inclination: | 74.0694° |
| perigee height: | 744 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 31.9758° |
| argument of perigee: | 137.8871° |
| revolutions per day: | 14.41019549 |
| mean anomaly at epoch: | 222.3431° |
| orbit number at epoch: | 27236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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