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 22175.83054054 .00000585 00000-0 11222-3 0 9994
2 27939 98.1927 316.5493 0013062 178.9559 181.1682 14.67368904 2125
| Epoch (UTC): | 24 June 2022 19:55:58 |
| Eccentricity: | 0.0013062 |
| inclination: | 98.1927° |
| perigee height: | 660 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 316.5493° |
| argument of perigee: | 178.9559° |
| revolutions per day: | 14.67368904 |
| mean anomaly at epoch: | 181.1682° |
| orbit number at epoch: | 212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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