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 25407U 98045B 23156.40259452 -.00000049 00000-0 -42954-6 0 9997
2 25407 71.0098 141.5052 0005663 134.8886 225.2698 14.15917748284365
Epoch (UTC): | 05 June 2023 09:39:44 |
Eccentricity: | 0.0005663 |
inclination: | 71.0098° |
perigee height: | 835 km |
apogee height: | 843 km |
right ascension of ascending node: | 141.5052° |
argument of perigee: | 134.8886° |
revolutions per day: | 14.15917748 |
mean anomaly at epoch: | 225.2698° |
orbit number at epoch: | 28436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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