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 42716U 98067LX 18316.95463152 .25568573 12659-4 27921-3 0 9996
2 42716 51.6101 291.3881 0002187 209.9477 150.8621 16.50348000 85401
| Epoch (UTC): | 12 November 2018 22:54:40 |
| Eccentricity: | 0.0002187 |
| inclination: | 51.6101° |
| perigee height: | 137 km |
| apogee height: | 140 km |
| right ascension of ascending node: | 291.3881° |
| argument of perigee: | 209.9477° |
| revolutions per day: | 16.50348000 |
| mean anomaly at epoch: | 150.8621° |
| orbit number at epoch: | 8540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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