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 25106U 97082C 13141.43805687 .00000146 00000-0 45053-4 0 2705
2 25106 086.3965 157.2409 0002344 116.6498 356.6623 14.34218327807123
| Epoch (UTC): | 21 May 2013 10:30:48 |
| Eccentricity: | 0.0002344 |
| inclination: | 86.3965° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 157.2409° |
| argument of perigee: | 116.6498° |
| revolutions per day: | 14.34218327 |
| mean anomaly at epoch: | 356.6623° |
| orbit number at epoch: | 80712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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