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 41933U 98067KV 18279.05129440 .08880754 12487-4 45483-3 0 9995
2 41933 51.6134 107.1518 0008522 281.0761 78.9308 16.42208149 98545
| Epoch (UTC): | 06 October 2018 01:13:51 |
| Eccentricity: | 0.0008522 |
| inclination: | 51.6134° |
| perigee height: | 154 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 107.1518° |
| argument of perigee: | 281.0761° |
| revolutions per day: | 16.42208149 |
| mean anomaly at epoch: | 78.9308° |
| orbit number at epoch: | 9854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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