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 40043U 14033AK 22177.79300545 .00000800 00000-0 12259-3 0 9994
2 40043 97.6561 6.5491 0060475 125.4341 235.2536 14.75027545431008
Epoch (UTC): | 26 June 2022 19:01:55 |
Eccentricity: | 0.0060475 |
inclination: | 97.6561° |
perigee height: | 602 km |
apogee height: | 687 km |
right ascension of ascending node: | 6.5491° |
argument of perigee: | 125.4341° |
revolutions per day: | 14.75027545 |
mean anomaly at epoch: | 235.2536° |
orbit number at epoch: | 43100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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