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 44874U 19092B 25132.09541892 .00000459 00000-0 10195-3 0 9996
2 44874 98.1528 321.0098 0009294 277.0381 82.9763 14.61542708287300
Epoch (UTC): | 12 May 2025 02:17:24 |
Eccentricity: | 0.0009294 |
inclination: | 98.1528° |
perigee height: | 681 km |
apogee height: | 695 km |
right ascension of ascending node: | 321.0098° |
argument of perigee: | 277.0381° |
revolutions per day: | 14.61542708 |
mean anomaly at epoch: | 82.9763° |
orbit number at epoch: | 28730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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