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 27422U 02021B 15025.55502043 .00000074 00000-0 45300-4 0 6982
2 27422 098.2739 062.1516 0011225 307.5288 207.4400 14.29126734661898
| Epoch (UTC): | 25 January 2015 13:19:13 |
| Eccentricity: | 0.0011225 |
| inclination: | 98.2739° |
| perigee height: | 786 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 62.1516° |
| argument of perigee: | 307.5288° |
| revolutions per day: | 14.29126734 |
| mean anomaly at epoch: | 207.4400° |
| orbit number at epoch: | 66189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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