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 18010U 87043F 19063.75218013 0.00000800 00000-0 83040-4 0 08
2 18010 63.3089 285.6302 0912626 55.4078 304.5922 13.45413932 02
| Epoch (UTC): | 04 March 2019 18:03:08 |
| Eccentricity: | 0.0912626 |
| inclination: | 63.3089° |
| perigee height: | 407 km |
| apogee height: | 1770 km |
| right ascension of ascending node: | 285.6302° |
| argument of perigee: | 55.4078° |
| revolutions per day: | 13.45413932 |
| mean anomaly at epoch: | 304.5922° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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