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 31144U 99025BGW 13276.33812043 +.00000206 +00000-0 +16243-3 0 9998
2 31144 099.2351 319.5653 0098724 273.1648 086.6520 14.00794070335052
| Epoch (UTC): | 03 October 2013 08:06:53 |
| Eccentricity: | 0.0098724 |
| inclination: | 99.2351° |
| perigee height: | 819 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 319.5653° |
| argument of perigee: | 273.1648° |
| revolutions per day: | 14.00794070 |
| mean anomaly at epoch: | 86.6520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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