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 00045U 60007A 23265.98733330 .00000627 00000-0 18208-3 0 9993
2 00045 66.6931 117.3010 0252463 169.0712 191.6023 14.34317445236800
Epoch (UTC): | 22 September 2023 23:41:45 |
Eccentricity: | 0.0252463 |
inclination: | 66.6931° |
perigee height: | 596 km |
apogee height: | 958 km |
right ascension of ascending node: | 117.3010° |
argument of perigee: | 169.0712° |
revolutions per day: | 14.34317445 |
mean anomaly at epoch: | 191.6023° |
orbit number at epoch: | 23680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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