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 25148U 98005A 10106.59199139 0.00001600 00000-0 00000-0 0 06
2 25148 64.4894 73.7808 7476396 245.5693 23.5855 2.00557566 00
| Epoch (UTC): | 16 April 2010 14:12:28 |
| Eccentricity: | 0.7476396 |
| inclination: | 64.4894° |
| perigee height: | 325 km |
| apogee height: | 40040 km |
| right ascension of ascending node: | 73.7808° |
| argument of perigee: | 245.5693° |
| revolutions per day: | 2.00557566 |
| mean anomaly at epoch: | 23.5855° |
| 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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