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 6153U 72065A 18171.90269708 +.00000015 +00000-0 +77255-5 0 9991
2 6153 035.0067 117.0745 0007105 200.7456 200.0959 14.57880467434455
| Epoch (UTC): | 20 June 2018 21:39:53 |
| Eccentricity: | 0.0007105 |
| inclination: | 35.0067° |
| perigee height: | 695 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 117.0745° |
| argument of perigee: | 200.7456° |
| revolutions per day: | 14.57880467 |
| mean anomaly at epoch: | 200.0959° |
| orbit number at epoch: | 43445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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