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 22141.42505443 .00002746 00000-0 35980-3 0 9996
2 39446 97.6836 106.6627 0068882 175.9784 184.1997 14.79477030456464
| Epoch (UTC): | 21 May 2022 10:12:04 |
| Eccentricity: | 0.0068882 |
| inclination: | 97.6836° |
| perigee height: | 583 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 106.6627° |
| argument of perigee: | 175.9784° |
| revolutions per day: | 14.79477030 |
| mean anomaly at epoch: | 184.1997° |
| orbit number at epoch: | 45646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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