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 42715U 98067LW 19125.26904075 .15894941 12567-4 41505-3 0 9994
2 42715 51.6151 127.9321 0004619 278.8566 95.8002 16.45622418112486
| Epoch (UTC): | 05 May 2019 06:27:25 |
| Eccentricity: | 0.0004619 |
| inclination: | 51.6151° |
| perigee height: | 148 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 127.9321° |
| argument of perigee: | 278.8566° |
| revolutions per day: | 16.45622418 |
| mean anomaly at epoch: | 95.8002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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