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 22179.53538632 .00009923 00000-0 29468-3 0 9996
2 41557 97.3889 277.2524 0009932 346.0351 137.3604 15.34940252339084
Epoch (UTC): | 28 June 2022 12:50:57 |
Eccentricity: | 0.0009932 |
inclination: | 97.3889° |
perigee height: | 454 km |
apogee height: | 468 km |
right ascension of ascending node: | 277.2524° |
argument of perigee: | 346.0351° |
revolutions per day: | 15.34940252 |
mean anomaly at epoch: | 137.3604° |
orbit number at epoch: | 33908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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