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 25042U 97069D 13142.44461254 .00000334 00000-0 11213-3 0 3316
2 25042 086.3956 283.5282 0002491 121.2103 238.9337 14.34219038813213
| Epoch (UTC): | 22 May 2013 10:40:14 |
| Eccentricity: | 0.0002491 |
| inclination: | 86.3956° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 283.5282° |
| argument of perigee: | 121.2103° |
| revolutions per day: | 14.34219038 |
| mean anomaly at epoch: | 238.9337° |
| orbit number at epoch: | 81321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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