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 8846U 76043B 22149.05870169 -.00000101 00000-0 -65382-4 0 9992
2 8846 81.2227 353.5428 0037224 319.3804 40.4589 14.08626345365447
Epoch (UTC): | 29 May 2022 01:24:31 |
Eccentricity: | 0.0037224 |
inclination: | 81.2227° |
perigee height: | 837 km |
apogee height: | 891 km |
right ascension of ascending node: | 353.5428° |
argument of perigee: | 319.3804° |
revolutions per day: | 14.08626345 |
mean anomaly at epoch: | 40.4589° |
orbit number at epoch: | 36544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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