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 29484U 06041F 08170.27591928 .21901596 31637-5 19690-3 0 9993
2 29484 098.2496 292.5583 0013872 275.6258 084.5236 16.51113477 98738
| Epoch (UTC): | 18 June 2008 06:37:19 |
| Eccentricity: | 0.0013872 |
| inclination: | 98.2496° |
| perigee height: | 127 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 292.5583° |
| argument of perigee: | 275.6258° |
| revolutions per day: | 16.51113477 |
| mean anomaly at epoch: | 84.5236° |
| orbit number at epoch: | 9873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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