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 40042U 14033AJ 25012.86852697 .00014644 00000-0 85555-3 0 9992
2 40042 98.0921 353.4517 0012322 135.6179 224.6039 15.11953905574417
Epoch (UTC): | 12 January 2025 20:50:40 |
Eccentricity: | 0.0012322 |
inclination: | 98.0921° |
perigee height: | 522 km |
apogee height: | 539 km |
right ascension of ascending node: | 353.4517° |
argument of perigee: | 135.6179° |
revolutions per day: | 15.11953905 |
mean anomaly at epoch: | 224.6039° |
orbit number at epoch: | 57441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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