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 41595U 16019B 17176.73956864 +.10739610 +12600-4 +40436-3 0 9991
2 41595 051.6070 299.8110 0008434 317.9127 042.8936 16.43514669058161
| Epoch (UTC): | 25 June 2017 17:44:58 |
| Eccentricity: | 0.0008434 |
| inclination: | 51.6070° |
| perigee height: | 151 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 299.8110° |
| argument of perigee: | 317.9127° |
| revolutions per day: | 16.43514669 |
| mean anomaly at epoch: | 42.8936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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