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 37662U 78026JZ 23334.78484096 .00001301 00000-0 69787-3 0 9993
2 37662 99.0248 328.2071 0034473 209.9056 150.0148 14.14537719535164
Epoch (UTC): | 30 November 2023 18:50:10 |
Eccentricity: | 0.0034473 |
inclination: | 99.0248° |
perigee height: | 819 km |
apogee height: | 869 km |
right ascension of ascending node: | 328.2071° |
argument of perigee: | 209.9056° |
revolutions per day: | 14.14537719 |
mean anomaly at epoch: | 150.0148° |
orbit number at epoch: | 53516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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