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 42717U 98067LY 19059.60577340 +.11886658 +12464-4 +71601-3 0 9999
2 42717 051.6020 100.2529 0001466 012.7224 347.7311 16.41511985101572
| Epoch (UTC): | 28 February 2019 14:32:18 |
| Eccentricity: | 0.0001466 |
| inclination: | 51.6020° |
| perigee height: | 161 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 100.2529° |
| argument of perigee: | 12.7224° |
| revolutions per day: | 16.41511985 |
| mean anomaly at epoch: | 347.7311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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