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 22178.01261946 .00000490 00000-0 95387-4 0 9997
2 27939 98.1923 318.7311 0013207 172.1809 187.9582 14.67370983 2447
| Epoch (UTC): | 27 June 2022 00:18:10 |
| Eccentricity: | 0.0013207 |
| inclination: | 98.1923° |
| perigee height: | 660 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 318.7311° |
| argument of perigee: | 172.1809° |
| revolutions per day: | 14.67370983 |
| mean anomaly at epoch: | 187.9582° |
| orbit number at epoch: | 244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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