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 23945U 96038A 10282.70677371 0.00000594 00000-0 00000-0 0 01
2 23945 63.9614 150.5143 7458398 246.7862 23.0699 2.00959734 00
| Epoch (UTC): | 09 October 2010 16:57:45 |
| Eccentricity: | 0.7458398 |
| inclination: | 63.9614° |
| perigee height: | 363 km |
| apogee height: | 39930 km |
| right ascension of ascending node: | 150.5143° |
| argument of perigee: | 246.7862° |
| revolutions per day: | 2.00959734 |
| mean anomaly at epoch: | 23.0699° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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