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 24317.86747450 .00001977 00000-0 50174-3 0 9994
2 00045 66.6933 96.9595 0256457 224.6157 133.4052 14.35120529296606
Epoch (UTC): | 12 November 2024 20:49:09 |
Eccentricity: | 0.0256457 |
inclination: | 66.6933° |
perigee height: | 591 km |
apogee height: | 958 km |
right ascension of ascending node: | 96.9595° |
argument of perigee: | 224.6157° |
revolutions per day: | 14.35120529 |
mean anomaly at epoch: | 133.4052° |
orbit number at epoch: | 29660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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