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 35498U 09036A 18112.74587951 +.00000034 +00000-0 +18062-3 0 9993
2 35498 082.4868 139.7638 0006674 189.1897 170.9060 12.40816997398437
| Epoch (UTC): | 22 April 2018 17:54:03 |
| Eccentricity: | 0.0006674 |
| inclination: | 82.4868° |
| perigee height: | 1498 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 139.7638° |
| argument of perigee: | 189.1897° |
| revolutions per day: | 12.40816997 |
| mean anomaly at epoch: | 170.9060° |
| orbit number at epoch: | 39843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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