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 42706U 98067LP 19128.42254485 .08245211 12410-4 57150-3 0 9990
2 42706 51.5998 109.6560 0003143 270.9046 228.4560 16.40380041113340
| Epoch (UTC): | 08 May 2019 10:08:27 |
| Eccentricity: | 0.0003143 |
| inclination: | 51.5998° |
| perigee height: | 163 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 109.6560° |
| argument of perigee: | 270.9046° |
| revolutions per day: | 16.40380041 |
| mean anomaly at epoch: | 228.4560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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