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 22179.92193576 .00000497 00000-0 96694-4 0 9990
2 27939 98.1926 320.6396 0013190 166.5061 193.6493 14.67373327 2724
| Epoch (UTC): | 28 June 2022 22:07:35 |
| Eccentricity: | 0.0013190 |
| inclination: | 98.1926° |
| perigee height: | 660 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 320.6396° |
| argument of perigee: | 166.5061° |
| revolutions per day: | 14.67373327 |
| mean anomaly at epoch: | 193.6493° |
| orbit number at epoch: | 272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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