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 25288U 98021D 13142.49406045 .00000151 00000-0 46808-4 0 2965
2 25288 086.3959 125.3203 0002397 107.2105 039.9498 14.34212637791923
| Epoch (UTC): | 22 May 2013 11:51:26 |
| Eccentricity: | 0.0002397 |
| inclination: | 86.3959° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 125.3203° |
| argument of perigee: | 107.2105° |
| revolutions per day: | 14.34212637 |
| mean anomaly at epoch: | 39.9498° |
| 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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