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 26061U 00004A 22222.17980313 .00000233 00000-0 89472-4 0 9993
2 26061 100.1997 290.0310 0032774 281.4819 78.2685 14.41723001184085
Epoch (UTC): | 10 August 2022 04:18:54 |
Eccentricity: | 0.0032774 |
inclination: | 100.1997° |
perigee height: | 729 km |
apogee height: | 776 km |
right ascension of ascending node: | 290.0310° |
argument of perigee: | 281.4819° |
revolutions per day: | 14.41723001 |
mean anomaly at epoch: | 78.2685° |
orbit number at epoch: | 18408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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