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 39446U 13066AG 23083.41101155 .00023032 00000-0 28401-2 0 9993
2 39446 97.7263 41.2388 0064476 255.8607 103.5436 14.81396724502462
| Epoch (UTC): | 24 March 2023 09:51:51 |
| Eccentricity: | 0.0064476 |
| inclination: | 97.7263° |
| perigee height: | 580 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 41.2388° |
| argument of perigee: | 255.8607° |
| revolutions per day: | 14.81396724 |
| mean anomaly at epoch: | 103.5436° |
| orbit number at epoch: | 50246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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