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 23079.15550385 .00005267 00000-0 65755-3 0 9996
2 39446 97.7247 37.1350 0064485 270.1859 89.1965 14.81316370501831
| Epoch (UTC): | 20 March 2023 03:43:55 |
| Eccentricity: | 0.0064485 |
| inclination: | 97.7247° |
| perigee height: | 580 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 37.1350° |
| argument of perigee: | 270.1859° |
| revolutions per day: | 14.81316370 |
| mean anomaly at epoch: | 89.1965° |
| orbit number at epoch: | 50183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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