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 42714U 98067LV 18265.92001965 +.06744984 +12188-4 +74906-3 0 9997
2 42714 051.6396 192.6696 0007557 179.7176 180.2695 16.36256502077350
| Epoch (UTC): | 22 September 2018 22:04:49 |
| Eccentricity: | 0.0007557 |
| inclination: | 51.6396° |
| perigee height: | 171 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 192.6696° |
| argument of perigee: | 179.7176° |
| revolutions per day: | 16.36256502 |
| mean anomaly at epoch: | 180.2695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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