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 27844U 03031E 20304.01328035 +.00000073 +00000-0 +52567-4 0 9992
2 27844 098.6831 309.7237 0010390 031.5744 328.6055 14.22264158899224
| Epoch (UTC): | 30 October 2020 00:19:07 |
| Eccentricity: | 0.0010390 |
| inclination: | 98.6831° |
| perigee height: | 810 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 309.7237° |
| argument of perigee: | 31.5744° |
| revolutions per day: | 14.22264158 |
| mean anomaly at epoch: | 328.6055° |
| orbit number at epoch: | 89922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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