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 43188U 18014J 23081.27155571 .00005609 00000-0 45880-3 0 9993
2 43188 97.6407 346.6733 0012633 91.0663 269.2008 14.99676198280525
| Epoch (UTC): | 22 March 2023 06:31:02 |
| Eccentricity: | 0.0012633 |
| inclination: | 97.6407° |
| perigee height: | 559 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 346.6733° |
| argument of perigee: | 91.0663° |
| revolutions per day: | 14.99676198 |
| mean anomaly at epoch: | 269.2008° |
| orbit number at epoch: | 28052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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