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 40014U 14033E 17145.81591937 +.00000875 +00000-0 +85314-4 0 9996
2 40014 097.9561 070.3169 0033222 041.8109 318.5643 14.94738784159863
| Epoch (UTC): | 25 May 2017 19:34:55 |
| Eccentricity: | 0.0033222 |
| inclination: | 97.9561° |
| perigee height: | 560 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 70.3169° |
| argument of perigee: | 41.8109° |
| revolutions per day: | 14.94738784 |
| mean anomaly at epoch: | 318.5643° |
| orbit number at epoch: | 15986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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