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 15063.82182633 .00000211 00000-0 99342-4 0 9995
2 27422 098.2689 098.4725 0012310 186.9180 173.1835 14.29143750667357
| Epoch (UTC): | 04 March 2015 19:43:25 |
| Eccentricity: | 0.0012310 |
| inclination: | 98.2689° |
| perigee height: | 786 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 98.4725° |
| argument of perigee: | 186.9180° |
| revolutions per day: | 14.29143750 |
| mean anomaly at epoch: | 173.1835° |
| orbit number at epoch: | 66735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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