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 24281.77019839 .00000591 00000-0 34835-3 0 9999
2 28352 71.0078 309.6374 0010210 351.8580 8.2374 14.12015174 47552
Epoch (UTC): | 07 October 2024 18:29:05 |
Eccentricity: | 0.0010210 |
inclination: | 71.0078° |
perigee height: | 845 km |
apogee height: | 860 km |
right ascension of ascending node: | 309.6374° |
argument of perigee: | 351.8580° |
revolutions per day: | 14.12015174 |
mean anomaly at epoch: | 8.2374° |
orbit number at epoch: | 4755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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