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 26474U 00047B 13143.53548780 .00001776 00000-0 18350-3 0 3092
2 26474 067.9975 328.5122 0060988 155.9289 204.4724 14.91274036693481
| Epoch (UTC): | 23 May 2013 12:51:06 |
| Eccentricity: | 0.0060988 |
| inclination: | 67.9975° |
| perigee height: | 551 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 328.5122° |
| argument of perigee: | 155.9289° |
| revolutions per day: | 14.91274036 |
| mean anomaly at epoch: | 204.4724° |
| orbit number at epoch: | 69348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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