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 21422U 91042A 13144.13558481 .00001066 00000-0 11017-3 0 5852
2 21422 082.5027 217.2892 0015092 199.3135 160.7514 14.89154438187249
| Epoch (UTC): | 24 May 2013 03:15:14 |
| Eccentricity: | 0.0015092 |
| inclination: | 82.5027° |
| perigee height: | 590 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 217.2892° |
| argument of perigee: | 199.3135° |
| revolutions per day: | 14.89154438 |
| mean anomaly at epoch: | 160.7514° |
| orbit number at epoch: | 18724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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