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 27840U 03031A 23154.52173959 .00000160 00000-0 62522-4 0 9992
2 27840 98.4784 119.9839 0099005 57.5402 303.5311 14.39153667 46448
Epoch (UTC): | 03 June 2023 12:31:18 |
Eccentricity: | 0.0099005 |
inclination: | 98.4784° |
perigee height: | 690 km |
apogee height: | 832 km |
right ascension of ascending node: | 119.9839° |
argument of perigee: | 57.5402° |
revolutions per day: | 14.39153667 |
mean anomaly at epoch: | 303.5311° |
orbit number at epoch: | 4644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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