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 42703U 98067LL 18126.44191986 .17722778 12425-4 13973-2 0 9990
2 42703 51.6180 185.5549 0005134 302.2194 57.7887 16.39284937 55666
| Epoch (UTC): | 06 May 2018 10:36:21 |
| Eccentricity: | 0.0005134 |
| inclination: | 51.6180° |
| perigee height: | 164 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 185.5549° |
| argument of perigee: | 302.2194° |
| revolutions per day: | 16.39284937 |
| mean anomaly at epoch: | 57.7887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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