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 is defined by the following mean orbital elements,
1 40284U 14065B 14296.61771037 -.00016976 -40384-4 00000+0 0 9991
2 40284 030.4737 296.6387 9755090 146.2479 349.5224 00.09145111 14964
| Epoch (UTC): | 23 October 2014 14:49:30 |
| Eccentricity: | 0.9755090 |
| inclination: | 30.4737° |
| perigee height: | -1282 km |
| apogee height: | 404724 km |
| right ascension of ascending node: | 296.6387° |
| argument of perigee: | 146.2479° |
| revolutions per day: | 0.09145111 |
| mean anomaly at epoch: | 349.5224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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