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 40012U 14033C 23085.92480003 .00003796 00000-0 54185-3 0 9993
2 40012 97.6686 264.0755 0055286 324.2588 35.4926 14.76240177471637
| Epoch (UTC): | 26 March 2023 22:11:42 |
| Eccentricity: | 0.0055286 |
| inclination: | 97.6686° |
| perigee height: | 602 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 264.0755° |
| argument of perigee: | 324.2588° |
| revolutions per day: | 14.76240177 |
| mean anomaly at epoch: | 35.4926° |
| orbit number at epoch: | 47163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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