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 28352U 04021A 25196.93236155 .00000362 00000-0 22296-3 0 9999
2 28352 71.0049 82.1304 0010875 270.2800 89.7075 14.12115304 87240
Epoch (UTC): | 15 July 2025 22:22:36 |
Eccentricity: | 0.0010875 |
inclination: | 71.0049° |
perigee height: | 844 km |
apogee height: | 860 km |
right ascension of ascending node: | 82.1304° |
argument of perigee: | 270.2800° |
revolutions per day: | 14.12115304 |
mean anomaly at epoch: | 89.7075° |
orbit number at epoch: | 8724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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