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 06155U 72065B 22144.58112272 .00001136 00000-0 17985-3 0 9992
2 06155 35.0035 102.3534 0038179 290.1231 69.5362 14.71957833636700
| Epoch (UTC): | 24 May 2022 13:56:49 |
| Eccentricity: | 0.0038179 |
| inclination: | 35.0035° |
| perigee height: | 628 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 102.3534° |
| argument of perigee: | 290.1231° |
| revolutions per day: | 14.71957833 |
| mean anomaly at epoch: | 69.5362° |
| orbit number at epoch: | 63670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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