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 35869U 09049E 17178.27431458 -.00000016 +00000-0 +11200-4 0 9997
2 35869 098.4138 198.7909 0005755 109.7026 250.4774 14.22369900403604
| Epoch (UTC): | 27 June 2017 06:35:00 |
| Eccentricity: | 0.0005755 |
| inclination: | 98.4138° |
| perigee height: | 813 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 198.7909° |
| argument of perigee: | 109.7026° |
| revolutions per day: | 14.22369900 |
| mean anomaly at epoch: | 250.4774° |
| orbit number at epoch: | 40360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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