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 39444U 13066AE 23080.87347386 .00005761 00000-0 65357-3 0 9997
2 39444 97.6625 48.1789 0053265 198.7052 161.2208 14.85674058502679
| Epoch (UTC): | 21 March 2023 20:57:48 |
| Eccentricity: | 0.0053265 |
| inclination: | 97.6625° |
| perigee height: | 574 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 48.1789° |
| argument of perigee: | 198.7052° |
| revolutions per day: | 14.85674058 |
| mean anomaly at epoch: | 161.2208° |
| orbit number at epoch: | 50267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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