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 00046U 60007B 23080.74148775 .00001815 00000-0 38183-3 0 9990
2 00046 66.6911 203.6421 0199901 100.2641 262.1073 14.50295432285104
| Epoch (UTC): | 21 March 2023 17:47:44 |
| Eccentricity: | 0.0199901 |
| inclination: | 66.6911° |
| perigee height: | 583 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 203.6421° |
| argument of perigee: | 100.2641° |
| revolutions per day: | 14.50295432 |
| mean anomaly at epoch: | 262.1073° |
| orbit number at epoch: | 28510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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