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 29228U 06021A 13144.48777854 .00001076 00000-0 94164-4 0 7760
2 29228 069.9368 270.1304 0002714 136.7294 346.7990 14.99924738385278
| Epoch (UTC): | 24 May 2013 11:42:24 |
| Eccentricity: | 0.0002714 |
| inclination: | 69.9368° |
| perigee height: | 565 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 270.1304° |
| argument of perigee: | 136.7294° |
| revolutions per day: | 14.99924738 |
| mean anomaly at epoch: | 346.7990° |
| orbit number at epoch: | 38527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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