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 28909U 05048B 18172.15911455 .00000040 00000-0 18398-3 0 9991
2 28909 82.4682 15.0306 0006507 186.5188 173.5815 12.55172891572588
| Epoch (UTC): | 21 June 2018 03:49:07 |
| Eccentricity: | 0.0006507 |
| inclination: | 82.4682° |
| perigee height: | 1438 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 15.0306° |
| argument of perigee: | 186.5188° |
| revolutions per day: | 12.55172891 |
| mean anomaly at epoch: | 173.5815° |
| orbit number at epoch: | 57258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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