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 26609U 00072B 21025.64966318 .00000017 00000-0 00000-0 0 9993
2 26609 9.1872 345.4054 7936239 219.5330 42.1739 1.25586135 92798
Epoch (UTC): | 25 January 2021 15:35:30 |
Eccentricity: | 0.7936239 |
inclination: | 9.1872° |
perigee height: | 1111 km |
apogee height: | 58710 km |
right ascension of ascending node: | 345.4054° |
argument of perigee: | 219.5330° |
revolutions per day: | 1.25586135 |
mean anomaly at epoch: | 42.1739° |
orbit number at epoch: | 9279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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