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 41672U 16046A 16238.56759634 +.00008390 +00000-0 +13289-3 0 9998
2 41672 051.6455 071.8205 0002923 237.0552 194.2778 15.54325716005979
| Epoch (UTC): | 25 August 2016 13:37:20 |
| Eccentricity: | 0.0002923 |
| inclination: | 51.6455° |
| perigee height: | 402 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 71.8205° |
| argument of perigee: | 237.0552° |
| revolutions per day: | 15.54325716 |
| mean anomaly at epoch: | 194.2778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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