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 25285U 98021A 13142.44653472 .00000158 00000-0 49404-4 0 3070
2 25285 086.3960 125.3804 0002278 106.8168 253.3278 14.34219825791925
| Epoch (UTC): | 22 May 2013 10:43:00 |
| Eccentricity: | 0.0002278 |
| inclination: | 86.3960° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 125.3804° |
| argument of perigee: | 106.8168° |
| revolutions per day: | 14.34219825 |
| mean anomaly at epoch: | 253.3278° |
| orbit number at epoch: | 79192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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