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 28485U 04047A 13145.82894163 .00003303 00000-0 24833-3 0 4477
2 28485 020.5586 018.5311 0013119 305.9314 139.6691 14.96309793465061
| Epoch (UTC): | 25 May 2013 19:53:40 |
| Eccentricity: | 0.0013119 |
| inclination: | 20.5586° |
| perigee height: | 569 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 18.5311° |
| argument of perigee: | 305.9314° |
| revolutions per day: | 14.96309793 |
| mean anomaly at epoch: | 139.6691° |
| orbit number at epoch: | 46506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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