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 24278U 96046B 24309.30585588 .00000042 00000-0 78637-4 0 9999
2 24278 98.5840 225.6044 0349929 185.1763 174.5720 13.53220042393631
Epoch (UTC): | 04 November 2024 07:20:25 |
Eccentricity: | 0.0349929 |
inclination: | 98.5840° |
perigee height: | 800 km |
apogee height: | 1321 km |
right ascension of ascending node: | 225.6044° |
argument of perigee: | 185.1763° |
revolutions per day: | 13.53220042 |
mean anomaly at epoch: | 174.5720° |
orbit number at epoch: | 39363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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