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 26960U 01049D 23149.65560895 .00005974 00000-0 31319-3 0 9995
2 26960 97.7836 180.3229 0045788 334.7738 25.1257 15.15259854181644
Epoch (UTC): | 29 May 2023 15:44:04 |
Eccentricity: | 0.0045788 |
inclination: | 97.7836° |
perigee height: | 488 km |
apogee height: | 552 km |
right ascension of ascending node: | 180.3229° |
argument of perigee: | 334.7738° |
revolutions per day: | 15.15259854 |
mean anomaly at epoch: | 25.1257° |
orbit number at epoch: | 18164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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