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 is defined by the following mean orbital elements,
1 04330U 70011A 03213.66651676 .11807697 -39564-5 77255-3 0 9992
2 04330 031.0024 211.0161 0012164 300.9584 059.5993 16.40190227435078
| Epoch (UTC): | 01 August 2003 15:59:47 |
| Eccentricity: | 0.0012164 |
| inclination: | 31.0024° |
| perigee height: | 157 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 211.0161° |
| argument of perigee: | 300.9584° |
| revolutions per day: | 16.40190227 |
| mean anomaly at epoch: | 59.5993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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