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 39130U 13015A 13138.98210593 .00002292 00000-0 12881-3 0 9997
2 39130 064.8766 300.0340 0078242 185.2934 174.7374 15.13569246 4447
| Epoch (UTC): | 18 May 2013 23:34:13 |
| Eccentricity: | 0.0078242 |
| inclination: | 64.8766° |
| perigee height: | 471 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 300.0340° |
| argument of perigee: | 185.2934° |
| revolutions per day: | 15.13569246 |
| mean anomaly at epoch: | 174.7374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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