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 20466U 90010B 25198.27517591 .00000385 00000-0 44064-4 0 9998
2 20466 82.5038 128.4433 0019914 0.4640 359.6589 14.83282212893580
Epoch (UTC): | 17 July 2025 06:36:15 |
Eccentricity: | 0.0019914 |
inclination: | 82.5038° |
perigee height: | 605 km |
apogee height: | 633 km |
right ascension of ascending node: | 128.4433° |
argument of perigee: | 0.4640° |
revolutions per day: | 14.83282212 |
mean anomaly at epoch: | 359.6589° |
orbit number at epoch: | 89358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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