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 23263.89543308 .00000514 00000-0 15407-3 0 9998
2 00045 66.6934 122.8197 0252672 170.6004 189.9961 14.34314311236501
Epoch (UTC): | 20 September 2023 21:29:25 |
Eccentricity: | 0.0252672 |
inclination: | 66.6934° |
perigee height: | 596 km |
apogee height: | 958 km |
right ascension of ascending node: | 122.8197° |
argument of perigee: | 170.6004° |
revolutions per day: | 14.34314311 |
mean anomaly at epoch: | 189.9961° |
orbit number at epoch: | 23650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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