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 28932U 06002B 13144.45352638 .00002407 00000-0 25778-3 0 3833
2 28932 098.3397 341.3038 0101139 113.6500 305.7207 14.86026596396827
| Epoch (UTC): | 24 May 2013 10:53:04 |
| Eccentricity: | 0.0101139 |
| inclination: | 98.3397° |
| perigee height: | 539 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 341.3038° |
| argument of perigee: | 113.6500° |
| revolutions per day: | 14.86026596 |
| mean anomaly at epoch: | 305.7207° |
| orbit number at epoch: | 39682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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