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 30586U 07005A 13223.10911614 0.00018000 00000-0 36604-3 0 02
2 30586 97.4244 359.8563 0001000 311.9054 48.0945 15.46309637 01
| Epoch (UTC): | 11 August 2013 02:37:07 |
| Eccentricity: | 0.0001000 |
| inclination: | 97.4244° |
| perigee height: | 427 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 359.8563° |
| argument of perigee: | 311.9054° |
| revolutions per day: | 15.46309637 |
| mean anomaly at epoch: | 48.0945° |
| 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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