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 25527U 98066A 13170.50368135 .00002089 00000-0 14973-3 0 7953
2 25527 085.5610 164.8800 0008162 009.5436 136.9057 15.03776598797565
| Epoch (UTC): | 19 June 2013 12:05:18 |
| Eccentricity: | 0.0008162 |
| inclination: | 85.5610° |
| perigee height: | 549 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 164.8800° |
| argument of perigee: | 9.5436° |
| revolutions per day: | 15.03776598 |
| mean anomaly at epoch: | 136.9057° |
| orbit number at epoch: | 79756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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