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 29050U 06011D 18231.79285515 .00000067 00000-0 24453-4 0 9996
2 29050 72.0173 326.3513 0048088 98.2363 262.4247 14.58691544659060
| Epoch (UTC): | 19 August 2018 19:01:42 |
| Eccentricity: | 0.0048088 |
| inclination: | 72.0173° |
| perigee height: | 663 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 326.3513° |
| argument of perigee: | 98.2363° |
| revolutions per day: | 14.58691544 |
| mean anomaly at epoch: | 262.4247° |
| orbit number at epoch: | 65906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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