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 28931U 06002A 21058.90919950 .00000219 00000-0 51568-4 0 9990
2 28931 97.8742 38.5208 0002118 42.1631 317.9747 14.62803093805048
| Epoch (UTC): | 27 February 2021 21:49:14 |
| Eccentricity: | 0.0002118 |
| inclination: | 97.8742° |
| perigee height: | 682 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 38.5208° |
| argument of perigee: | 42.1631° |
| revolutions per day: | 14.62803093 |
| mean anomaly at epoch: | 317.9747° |
| orbit number at epoch: | 80504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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