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 25406U 98045A 13143.80067689 -.00000221 00000-0 -93185-4 0 9783
2 25406 070.8305 270.4340 0006762 244.5150 260.2009 14.12397893764388
| Epoch (UTC): | 23 May 2013 19:12:58 |
| Eccentricity: | 0.0006762 |
| inclination: | 70.8305° |
| perigee height: | 846 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 270.4340° |
| argument of perigee: | 244.5150° |
| revolutions per day: | 14.12397893 |
| mean anomaly at epoch: | 260.2009° |
| orbit number at epoch: | 76438 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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