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 13143.39209551 .00000309 00000-0 10342-3 0 3354
2 25276 086.3981 188.0514 0002375 108.2039 251.9416 14.34218874793106
| Epoch (UTC): | 23 May 2013 09:24:37 |
| Eccentricity: | 0.0002375 |
| inclination: | 86.3981° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 188.0514° |
| argument of perigee: | 108.2039° |
| revolutions per day: | 14.34218874 |
| mean anomaly at epoch: | 251.9416° |
| orbit number at epoch: | 79310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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