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 14068.33818206 .00000487 00000-0 31407-3 0 1471
2 15392 021.4948 015.1493 1034837 331.4784 203.1014 12.45379974334809
| Epoch (UTC): | 09 March 2014 08:06:58 |
| Eccentricity: | 0.1034837 |
| inclination: | 21.4948° |
| perigee height: | 670 km |
| apogee height: | 2297 km |
| right ascension of ascending node: | 15.1493° |
| argument of perigee: | 331.4784° |
| revolutions per day: | 12.45379974 |
| mean anomaly at epoch: | 203.1014° |
| orbit number at epoch: | 33480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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