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 6155U 72065B 22139.69734811 .00001185 00000-0 18744-3 0 9995
2 6155 35.0027 130.7156 0038183 250.1430 109.5151 14.71946717656890
| Epoch (UTC): | 19 May 2022 16:44:10 |
| Eccentricity: | 0.0038183 |
| inclination: | 35.0027° |
| perigee height: | 628 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 130.7156° |
| argument of perigee: | 250.1430° |
| revolutions per day: | 14.71946717 |
| mean anomaly at epoch: | 109.5151° |
| orbit number at epoch: | 65689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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