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 42466U 10057BF 19121.81527925 -.00000368 00000-0 -18714-2 0 9990
2 42466 20.6919 305.5417 7200207 285.3388 10.8191 2.18727697 30542
| Epoch (UTC): | 01 May 2019 19:34:00 |
| Eccentricity: | 0.7200207 |
| inclination: | 20.6919° |
| perigee height: | 640 km |
| apogee height: | 36740 km |
| right ascension of ascending node: | 305.5417° |
| argument of perigee: | 285.3388° |
| revolutions per day: | 2.18727697 |
| mean anomaly at epoch: | 10.8191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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