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 40719U 15032E 25108.57456386 .00010145 00000-0 90997-3 0 9990
2 40719 97.6499 329.3656 0010896 193.3728 166.7206 14.95900426527606
Epoch (UTC): | 18 April 2025 13:47:22 |
Eccentricity: | 0.0010896 |
inclination: | 97.6499° |
perigee height: | 572 km |
apogee height: | 587 km |
right ascension of ascending node: | 329.3656° |
argument of perigee: | 193.3728° |
revolutions per day: | 14.95900426 |
mean anomaly at epoch: | 166.7206° |
orbit number at epoch: | 52760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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