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 25510U 98061C 16272.09447730 .00000333 00000-0 45785-4 0 9991
2 25510 31.4356 203.3661 0328761 276.9587 193.6890 14.37078729939587
| Epoch (UTC): | 28 September 2016 02:16:02 |
| Eccentricity: | 0.0328761 |
| inclination: | 31.4356° |
| perigee height: | 533 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 203.3661° |
| argument of perigee: | 276.9587° |
| revolutions per day: | 14.37078729 |
| mean anomaly at epoch: | 193.6890° |
| orbit number at epoch: | 93958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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