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 22825U 93061C 13142.79255275 .00000116 00000-0 62367-4 0 3890
2 22825 098.6167 087.0875 0008340 011.4210 021.2971 14.29562259 25001
| Epoch (UTC): | 22 May 2013 19:01:16 |
| Eccentricity: | 0.0008340 |
| inclination: | 98.6167° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 87.0875° |
| argument of perigee: | 11.4210° |
| revolutions per day: | 14.29562259 |
| mean anomaly at epoch: | 21.2971° |
| orbit number at epoch: | 2500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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