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 22803U 93059B 14112.49246894 -.00000200 00000-0 -75698-4 0 2554
2 22803 070.9890 156.1433 0018534 332.9165 027.0989 14.16663894 65164
| Epoch (UTC): | 22 April 2014 11:49:09 |
| Eccentricity: | 0.0018534 |
| inclination: | 70.9890° |
| perigee height: | 823 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 156.1433° |
| argument of perigee: | 332.9165° |
| revolutions per day: | 14.16663894 |
| mean anomaly at epoch: | 27.0989° |
| orbit number at epoch: | 6516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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