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 46U 60007B 23026.32558487 .00000854 00000-0 19125-3 0 9996
2 46 66.6914 350.8655 0203434 142.2029 219.3569 14.50063608277208
| Epoch (UTC): | 26 January 2023 07:48:50 |
| Eccentricity: | 0.0203434 |
| inclination: | 66.6914° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 350.8655° |
| argument of perigee: | 142.2029° |
| revolutions per day: | 14.50063608 |
| mean anomaly at epoch: | 219.3569° |
| orbit number at epoch: | 27720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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