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 16495U 86006A 13138.04945831 .00005395 00000-0 31464-3 0 900
2 16495 082.4767 114.4183 0016672 348.4257 077.2389 15.11655636490051
| Epoch (UTC): | 18 May 2013 01:11:13 |
| Eccentricity: | 0.0016672 |
| inclination: | 82.4767° |
| perigee height: | 519 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 114.4183° |
| argument of perigee: | 348.4257° |
| revolutions per day: | 15.11655636 |
| mean anomaly at epoch: | 77.2389° |
| orbit number at epoch: | 49005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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