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 28395U 04031C 25187.88282719 .00005843 00000-0 69464-3 0 9995
2 28395 49.4816 3.8639 5183341 190.6790 151.7065 5.34413206386142
Epoch (UTC): | 06 July 2025 21:11:16 |
Eccentricity: | 0.5183341 |
inclination: | 49.4816° |
perigee height: | 278 km |
apogee height: | 14604 km |
right ascension of ascending node: | 3.8639° |
argument of perigee: | 190.6790° |
revolutions per day: | 5.34413206 |
mean anomaly at epoch: | 151.7065° |
orbit number at epoch: | 38614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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