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 40912U 15049P 22179.08485899 .00008616 00000-0 33436-3 0 9990
2 40912 97.4358 190.4356 0010617 263.9374 168.0747 15.26298598375374
Epoch (UTC): | 28 June 2022 02:02:11 |
Eccentricity: | 0.0010617 |
inclination: | 97.4358° |
perigee height: | 479 km |
apogee height: | 494 km |
right ascension of ascending node: | 190.4356° |
argument of perigee: | 263.9374° |
revolutions per day: | 15.26298598 |
mean anomaly at epoch: | 168.0747° |
orbit number at epoch: | 37537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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