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 25063U 97074A 15166.76390326 .03950263 00000-0 41679-3 0 9996
2 25063 034.9372 203.9770 0001344 140.8634 219.2792 16.36482121 1874
| Epoch (UTC): | 15 June 2015 18:20:01 |
| Eccentricity: | 0.0001344 |
| inclination: | 34.9372° |
| perigee height: | 174 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 203.9770° |
| argument of perigee: | 140.8634° |
| revolutions per day: | 16.36482121 |
| mean anomaly at epoch: | 219.2792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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