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 13169.13144101 .00000484 00000-0 48467-4 0 6077
2 21422 082.5008 193.6106 0016813 121.0035 239.2838 14.89187707190965
| Epoch (UTC): | 18 June 2013 03:09:16 |
| Eccentricity: | 0.0016813 |
| inclination: | 82.5008° |
| perigee height: | 589 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 193.6106° |
| argument of perigee: | 121.0035° |
| revolutions per day: | 14.89187707 |
| mean anomaly at epoch: | 239.2838° |
| orbit number at epoch: | 19096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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