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 41931U 98067KT 17290.98270503 .14164078 12479-4 76733-3 0 9998
2 41931 51.6104 115.9004 0006182 280.1451 79.8879 16.42240901 42996
| Epoch (UTC): | 17 October 2017 23:35:05 |
| Eccentricity: | 0.0006182 |
| inclination: | 51.6104° |
| perigee height: | 156 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 115.9004° |
| argument of perigee: | 280.1451° |
| revolutions per day: | 16.42240901 |
| mean anomaly at epoch: | 79.8879° |
| orbit number at epoch: | 4299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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