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 36104U 09066A 13135.90218484 0.00000000 00000-0 00000-0 0 07
2 36104 97.7579 211.2273 0004000 41.0719 318.9280 14.93425629 00
| Epoch (UTC): | 15 May 2013 21:39:08 |
| Eccentricity: | 0.0004000 |
| inclination: | 97.7579° |
| perigee height: | 584 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 211.2273° |
| argument of perigee: | 41.0719° |
| revolutions per day: | 14.93425629 |
| mean anomaly at epoch: | 318.9280° |
| 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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