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 32164U 99025CTJ 15072.08990585 .00002255 00000-0 55693-3 0 9995
2 32164 99.3273 29.7416 0124038 216.0851 143.1921 14.48733747405009
| Epoch (UTC): | 13 March 2015 02:09:27 |
| Eccentricity: | 0.0124038 |
| inclination: | 99.3273° |
| perigee height: | 641 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 29.7416° |
| argument of perigee: | 216.0851° |
| revolutions per day: | 14.48733747 |
| mean anomaly at epoch: | 143.1921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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