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 25544U 98067A 13170.94447557 -.00054488 00000-0 00000+0 0 324
2 25544 051.6483 094.6612 0016678 094.4658 265.8781 15.50659641239239
| Epoch (UTC): | 19 June 2013 22:40:02 |
| Eccentricity: | 0.0016678 |
| inclination: | 51.6483° |
| perigee height: | 403 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 94.6612° |
| argument of perigee: | 94.4658° |
| revolutions per day: | 15.50659641 |
| mean anomaly at epoch: | 265.8781° |
| orbit number at epoch: | 23923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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