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 15025.33180665 .00000352 00000-0 11850-3 0 1365
2 25276 086.3972 292.2821 0002045 099.1642 260.9785 14.34221011880818
| Epoch (UTC): | 25 January 2015 07:57:48 |
| Eccentricity: | 0.0002045 |
| inclination: | 86.3972° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 292.2821° |
| argument of perigee: | 99.1642° |
| revolutions per day: | 14.34221011 |
| mean anomaly at epoch: | 260.9785° |
| orbit number at epoch: | 88081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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