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 25169U 98010A 13139.44320080 .00000415 00000-0 14110-3 0 552
2 25169 086.3978 252.9871 0002302 109.3650 294.2104 14.34219963798256
| Epoch (UTC): | 19 May 2013 10:38:12 |
| Eccentricity: | 0.0002302 |
| inclination: | 86.3978° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 252.9871° |
| argument of perigee: | 109.3650° |
| revolutions per day: | 14.34219963 |
| mean anomaly at epoch: | 294.2104° |
| orbit number at epoch: | 79825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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