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 41895U 98067KR 18061.52581171 .12025536 12682-4 40347-3 0 9991
2 41895 51.6547 142.6546 0011212 346.6197 16.6343 16.43666377 68734
| Epoch (UTC): | 02 March 2018 12:37:10 |
| Eccentricity: | 0.0011212 |
| inclination: | 51.6547° |
| perigee height: | 149 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 142.6546° |
| argument of perigee: | 346.6197° |
| revolutions per day: | 16.43666377 |
| mean anomaly at epoch: | 16.6343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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