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 29507U 06046C 25200.45815612 .00003678 00000-0 20304-3 0 9996
2 29507 97.5938 240.9887 0035100 356.6906 3.4088 15.14052664 24764
Epoch (UTC): | 19 July 2025 10:59:44 |
Eccentricity: | 0.0035100 |
inclination: | 97.5938° |
perigee height: | 499 km |
apogee height: | 548 km |
right ascension of ascending node: | 240.9887° |
argument of perigee: | 356.6906° |
revolutions per day: | 15.14052664 |
mean anomaly at epoch: | 3.4088° |
orbit number at epoch: | 2476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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