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 37854U 11061E 13169.14868451 .00003514 00000-0 26461-3 0 5253
2 37854 101.7178 024.0978 0234925 023.4187 092.5580 14.84410882 88605
| Epoch (UTC): | 18 June 2013 03:34:06 |
| Eccentricity: | 0.0234925 |
| inclination: | 101.7178° |
| perigee height: | 451 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 24.0978° |
| argument of perigee: | 23.4187° |
| revolutions per day: | 14.84410882 |
| mean anomaly at epoch: | 92.5580° |
| orbit number at epoch: | 8860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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