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 23466U 95002D 13167.90497028 .00000024 00000-0 92563-5 0 6054
2 23466 082.9265 269.6243 0033378 310.8142 187.6357 13.74250946922573
| Epoch (UTC): | 16 June 2013 21:43:09 |
| Eccentricity: | 0.0033378 |
| inclination: | 82.9265° |
| perigee height: | 960 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 269.6243° |
| argument of perigee: | 310.8142° |
| revolutions per day: | 13.74250946 |
| mean anomaly at epoch: | 187.6357° |
| orbit number at epoch: | 92257 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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