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 26473U 00047A 13154.12243964 0.00000500 00000-0 93052-4 0 09
2 26473 68.0114 52.6733 0009000 338.7131 21.2869 14.64981422 04
| Epoch (UTC): | 03 June 2013 02:56:18 |
| Eccentricity: | 0.0009000 |
| inclination: | 68.0114° |
| perigee height: | 671 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 52.6733° |
| argument of perigee: | 338.7131° |
| revolutions per day: | 14.64981422 |
| mean anomaly at epoch: | 21.2869° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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