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 36575U 10020C 10172.70653775 .99999999 -60602-5 75369-3 0 9995
2 36575 029.9702 005.8364 0011956 035.9119 324.7358 16.63263503 5106
| Epoch (UTC): | 21 June 2010 16:57:24 |
| Eccentricity: | 0.0011956 |
| inclination: | 29.9702° |
| perigee height: | 97 km |
| apogee height: | 112 km |
| right ascension of ascending node: | 5.8364° |
| argument of perigee: | 35.9119° |
| revolutions per day: | 16.63263503 |
| mean anomaly at epoch: | 324.7358° |
| orbit number at epoch: | 510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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