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 20453U 90008B 13144.16338603 .00009667 00000-0 66132-3 0 6855
2 20453 035.6280 235.8552 0344605 169.6061 191.2000 14.67990464228499
| Epoch (UTC): | 24 May 2013 03:55:16 |
| Eccentricity: | 0.0344605 |
| inclination: | 35.6280° |
| perigee height: | 425 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 235.8552° |
| argument of perigee: | 169.6061° |
| revolutions per day: | 14.67990464 |
| mean anomaly at epoch: | 191.2000° |
| orbit number at epoch: | 22849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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