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 35658U 93036ANZ 24225.31276556 .00189856 00000-0 21019-1 0 9999
2 35658 74.0067 207.1536 0005344 349.8331 10.2739 14.86198823806785
Epoch (UTC): | 12 August 2024 07:30:22 |
Eccentricity: | 0.0005344 |
inclination: | 74.0067° |
perigee height: | 606 km |
apogee height: | 613 km |
right ascension of ascending node: | 207.1536° |
argument of perigee: | 349.8331° |
revolutions per day: | 14.86198823 |
mean anomaly at epoch: | 10.2739° |
orbit number at epoch: | 80678 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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