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 27939U 03042A 22176.98977014 .00000552 00000-0 10646-3 0 9994
2 27939 98.1924 317.7082 0013135 175.2997 184.8311 14.67370113 2298
| Epoch (UTC): | 25 June 2022 23:45:16 |
| Eccentricity: | 0.0013135 |
| inclination: | 98.1924° |
| perigee height: | 660 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 317.7082° |
| argument of perigee: | 175.2997° |
| revolutions per day: | 14.67370113 |
| mean anomaly at epoch: | 184.8311° |
| orbit number at epoch: | 229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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