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 25276U 98019E 15062.30914104 .00000235 00000-0 76693-4 0 9990
2 25276 086.3926 276.8202 0001973 088.2453 271.8969 14.34216521886110
| Epoch (UTC): | 03 March 2015 07:25:09 |
| Eccentricity: | 0.0001973 |
| inclination: | 86.3926° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 276.8202° |
| argument of perigee: | 88.2453° |
| revolutions per day: | 14.34216521 |
| mean anomaly at epoch: | 271.8969° |
| orbit number at epoch: | 88611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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