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 15944U 85069A 24278.87649379 .00074362 00000-0 13835-2 0 9991
2 15944 82.4918 87.2273 0009422 136.4377 223.7619 15.48538758143703
Epoch (UTC): | 04 October 2024 21:02:09 |
Eccentricity: | 0.0009422 |
inclination: | 82.4918° |
perigee height: | 414 km |
apogee height: | 427 km |
right ascension of ascending node: | 87.2273° |
argument of perigee: | 136.4377° |
revolutions per day: | 15.48538758 |
mean anomaly at epoch: | 223.7619° |
orbit number at epoch: | 14370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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