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 26998U 01055B 21061.46418854 .00000169 00000-0 22311-4 0 9994
2 26998 74.0727 139.5475 0001299 231.3109 128.7956 14.88275076 42920
Epoch (UTC): | 02 March 2021 11:08:25 |
Eccentricity: | 0.0001299 |
inclination: | 74.0727° |
perigee height: | 602 km |
apogee height: | 604 km |
right ascension of ascending node: | 139.5475° |
argument of perigee: | 231.3109° |
revolutions per day: | 14.88275076 |
mean anomaly at epoch: | 128.7956° |
orbit number at epoch: | 4292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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