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 40069U 14037A 25138.23373035 .00000180 00000-0 10188-3 0 9999
2 40069 98.4671 124.0907 0006967 101.6677 258.5283 14.21290546563219
Epoch (UTC): | 18 May 2025 05:36:34 |
Eccentricity: | 0.0006967 |
inclination: | 98.4671° |
perigee height: | 816 km |
apogee height: | 826 km |
right ascension of ascending node: | 124.0907° |
argument of perigee: | 101.6677° |
revolutions per day: | 14.21290546 |
mean anomaly at epoch: | 258.5283° |
orbit number at epoch: | 56321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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