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 25260U 98017A 13142.73602543 .00000135 00000-0 82022-4 0 5523
2 25260 098.5129 198.7024 0001750 073.5343 286.6013 14.20894976786085
| Epoch (UTC): | 22 May 2013 17:39:52 |
| Eccentricity: | 0.0001750 |
| inclination: | 98.5129° |
| perigee height: | 821 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 198.7024° |
| argument of perigee: | 73.5343° |
| revolutions per day: | 14.20894976 |
| mean anomaly at epoch: | 286.6013° |
| orbit number at epoch: | 78608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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