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 41557U 16033B 22177.12272056 .00010621 00000-0 31566-3 0 9993
2 41557 97.3883 274.8340 0010042 355.1572 125.2121 15.34894825338710
Epoch (UTC): | 26 June 2022 02:56:43 |
Eccentricity: | 0.0010042 |
inclination: | 97.3883° |
perigee height: | 454 km |
apogee height: | 468 km |
right ascension of ascending node: | 274.8340° |
argument of perigee: | 355.1572° |
revolutions per day: | 15.34894825 |
mean anomaly at epoch: | 125.2121° |
orbit number at epoch: | 33871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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