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 28646U 05016A 13138.67373285 0.00000100 00000-0 23797-4 0 01
2 28646 57.0140 294.5006 0007000 45.4025 314.5974 14.53509706 01
| Epoch (UTC): | 18 May 2013 16:10:10 |
| Eccentricity: | 0.0007000 |
| inclination: | 57.0140° |
| perigee height: | 709 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 294.5006° |
| argument of perigee: | 45.4025° |
| revolutions per day: | 14.53509706 |
| mean anomaly at epoch: | 314.5974° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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