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 11239U 79003B 15030.88183809 .00000000 00000-0 -15077-4 0 4269
2 11239 082.9394 013.0433 0039389 298.7350 122.3339 13.75755879808469
| Epoch (UTC): | 30 January 2015 21:09:50 |
| Eccentricity: | 0.0039389 |
| inclination: | 82.9394° |
| perigee height: | 950 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 13.0433° |
| argument of perigee: | 298.7350° |
| revolutions per day: | 13.75755879 |
| mean anomaly at epoch: | 122.3339° |
| orbit number at epoch: | 80846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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