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 data is extracted from the following two-line orbital elements,
1 15392U 84115B 16272.86198728 +.00000117 +00000-0 -25973-4 0 9996
2 15392 021.4914 065.2642 1034581 048.9617 319.5715 12.45534554433611
| Epoch (UTC): | 28 September 2016 20:41:15 |
| Eccentricity: | 0.1034581 |
| inclination: | 21.4914° |
| perigee height: | 670 km |
| apogee height: | 2296 km |
| right ascension of ascending node: | 65.2642° |
| argument of perigee: | 48.9617° |
| revolutions per day: | 12.45534554 |
| mean anomaly at epoch: | 319.5715° |
| orbit number at epoch: | 43361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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