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 42053U 17009A 17077.58008207 +.00001743 +00000-0 +33487-4 0 9997
2 42053 051.6421 129.9559 0006873 308.4095 172.2983 15.54222926047661
| Epoch (UTC): | 18 March 2017 13:55:19 |
| Eccentricity: | 0.0006873 |
| inclination: | 51.6421° |
| perigee height: | 400 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 129.9559° |
| argument of perigee: | 308.4095° |
| revolutions per day: | 15.54222926 |
| mean anomaly at epoch: | 172.2983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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