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 32958U 08026A 14069.72375129 .00000164 00000-0 97825-4 0 7915
2 32958 098.5683 131.8282 0010051 137.0079 223.1876 14.19421123299879
| Epoch (UTC): | 10 March 2014 17:22:12 |
| Eccentricity: | 0.0010051 |
| inclination: | 98.5683° |
| perigee height: | 820 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 131.8282° |
| argument of perigee: | 137.0079° |
| revolutions per day: | 14.19421123 |
| mean anomaly at epoch: | 223.1876° |
| orbit number at epoch: | 29987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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