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 22175.81808821 .00011696 00000-0 34753-3 0 9996
2 41557 97.3879 273.5266 0010247 359.5940 116.6262 15.34873050338517
Epoch (UTC): | 24 June 2022 19:38:02 |
Eccentricity: | 0.0010247 |
inclination: | 97.3879° |
perigee height: | 454 km |
apogee height: | 468 km |
right ascension of ascending node: | 273.5266° |
argument of perigee: | 359.5940° |
revolutions per day: | 15.34873050 |
mean anomaly at epoch: | 116.6262° |
orbit number at epoch: | 33851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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