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 42097U 81053PH 24272.92631004 .00009993 00000-0 46946-2 0 9992
2 42097 82.8091 151.1300 0064190 52.6459 308.0544 14.18858484102439
Epoch (UTC): | 28 September 2024 22:13:53 |
Eccentricity: | 0.0064190 |
inclination: | 82.8091° |
perigee height: | 783 km |
apogee height: | 875 km |
right ascension of ascending node: | 151.1300° |
argument of perigee: | 52.6459° |
revolutions per day: | 14.18858484 |
mean anomaly at epoch: | 308.0544° |
orbit number at epoch: | 10243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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