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 23083.53872108 .00001791 00000-0 55884-3 0 9990
2 26061 100.1880 199.8229 0033074 358.3361 1.7708 14.42118964216700
Epoch (UTC): | 24 March 2023 12:55:45 |
Eccentricity: | 0.0033074 |
inclination: | 100.1880° |
perigee height: | 728 km |
apogee height: | 775 km |
right ascension of ascending node: | 199.8229° |
argument of perigee: | 358.3361° |
revolutions per day: | 14.42118964 |
mean anomaly at epoch: | 1.7708° |
orbit number at epoch: | 21670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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