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 40069U 14037A 22179.52119192 .00000006 00000-0 22018-4 0 9998
2 40069 98.4305 196.8206 0004591 298.5151 61.5570 14.20711809413434
Epoch (UTC): | 28 June 2022 12:30:30 |
Eccentricity: | 0.0004591 |
inclination: | 98.4305° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 196.8206° |
argument of perigee: | 298.5151° |
revolutions per day: | 14.20711809 |
mean anomaly at epoch: | 61.5570° |
orbit number at epoch: | 41343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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