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 is defined by the following mean orbital elements,
1 41939U 98067KZ 18011.28402027 +.11925055 +12489-4 +54124-3 0 9997
2 41939 051.6147 038.9582 0001091 231.1728 128.9202 16.43639489055773
| Epoch (UTC): | 11 January 2018 06:48:59 |
| Eccentricity: | 0.0001091 |
| inclination: | 51.6147° |
| perigee height: | 155 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 38.9582° |
| argument of perigee: | 231.1728° |
| revolutions per day: | 16.43639489 |
| mean anomaly at epoch: | 128.9202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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