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 40021U 14033M 22179.13118477 .00002168 00000-0 21446-3 0 9998
2 40021 98.0127 129.5259 0012859 13.1637 346.9915 14.92929791436299
Epoch (UTC): | 28 June 2022 03:08:54 |
Eccentricity: | 0.0012859 |
inclination: | 98.0127° |
perigee height: | 580 km |
apogee height: | 598 km |
right ascension of ascending node: | 129.5259° |
argument of perigee: | 13.1637° |
revolutions per day: | 14.92929791 |
mean anomaly at epoch: | 346.9915° |
orbit number at epoch: | 43629 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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