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 28095U 03054A 13142.97469217 0.00000000 00000-0 00000-0 0 05
2 28095 63.4310 143.0812 0171000 359.4070 0.5930 13.40652688 09
| Epoch (UTC): | 22 May 2013 23:23:33 |
| Eccentricity: | 0.0171000 |
| inclination: | 63.4310° |
| perigee height: | 979 km |
| apogee height: | 1235 km |
| right ascension of ascending node: | 143.0812° |
| argument of perigee: | 359.4070° |
| revolutions per day: | 13.40652688 |
| mean anomaly at epoch: | 0.5930° |
| 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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