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 data is extracted from the following two-line orbital elements,
1 42721U 98067MA 18224.59980250 +.12090849 +12543-4 +42456-3 0 9997
2 42721 051.6121 042.1184 0010981 284.9336 075.0476 16.43490172069841
| Epoch (UTC): | 12 August 2018 14:23:42 |
| Eccentricity: | 0.0010981 |
| inclination: | 51.6121° |
| perigee height: | 149 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 42.1184° |
| argument of perigee: | 284.9336° |
| revolutions per day: | 16.43490172 |
| mean anomaly at epoch: | 75.0476° |
| orbit number at epoch: | 6984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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