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 23657U 95046A 13142.15602690 .00000805 00000-0 95282-4 0 250
2 23657 082.5290 215.4765 0021786 318.7182 041.2385 14.83234165956814
| Epoch (UTC): | 22 May 2013 03:44:40 |
| Eccentricity: | 0.0021786 |
| inclination: | 82.5290° |
| perigee height: | 604 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 215.4765° |
| argument of perigee: | 318.7182° |
| revolutions per day: | 14.83234165 |
| mean anomaly at epoch: | 41.2385° |
| orbit number at epoch: | 95681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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