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 13139.19335648 .00000875 00000-0 78053-4 0 7601
2 29228 069.9364 283.5536 0003082 148.8890 194.3917 14.99911416384470
| Epoch (UTC): | 19 May 2013 04:38:26 |
| Eccentricity: | 0.0003082 |
| inclination: | 69.9364° |
| perigee height: | 565 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 283.5536° |
| argument of perigee: | 148.8890° |
| revolutions per day: | 14.99911416 |
| mean anomaly at epoch: | 194.3917° |
| orbit number at epoch: | 38447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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