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 42820U 98067MU 19123.10626650 .20777511 12651-4 37226-3 0 9990
2 42820 51.6051 142.7539 0005305 301.2009 59.2873 16.47402492104441
| Epoch (UTC): | 03 May 2019 02:33:01 |
| Eccentricity: | 0.0005305 |
| inclination: | 51.6051° |
| perigee height: | 143 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 142.7539° |
| argument of perigee: | 301.2009° |
| revolutions per day: | 16.47402492 |
| mean anomaly at epoch: | 59.2873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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