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 27598U 02056B 18347.81983221 +.00000007 +00000-0 +19623-4 0 9993
2 27598 098.5071 292.7000 0010280 083.1484 277.0867 14.28670991834090
| Epoch (UTC): | 13 December 2018 19:40:33 |
| Eccentricity: | 0.0010280 |
| inclination: | 98.5071° |
| perigee height: | 789 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 292.7000° |
| argument of perigee: | 83.1484° |
| revolutions per day: | 14.28670991 |
| mean anomaly at epoch: | 277.0867° |
| orbit number at epoch: | 83409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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