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 21575U 91050B 23273.46752652 .00000389 00000-0 13387-3 0 9994
2 21575 98.4730 340.5354 0006091 279.9710 80.0791 14.41353671691970
Epoch (UTC): | 30 September 2023 11:13:14 |
Eccentricity: | 0.0006091 |
inclination: | 98.4730° |
perigee height: | 749 km |
apogee height: | 758 km |
right ascension of ascending node: | 340.5354° |
argument of perigee: | 279.9710° |
revolutions per day: | 14.41353671 |
mean anomaly at epoch: | 80.0791° |
orbit number at epoch: | 69197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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