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 14445U 77121BH 24358.16834474 .00024517 00000-0 67860-2 0 9993
2 14445 66.4692 270.9504 0064379 126.0544 234.6548 14.45364568113701
Epoch (UTC): | 23 December 2024 04:02:24 |
Eccentricity: | 0.0064379 |
inclination: | 66.4692° |
perigee height: | 695 km |
apogee height: | 786 km |
right ascension of ascending node: | 270.9504° |
argument of perigee: | 126.0544° |
revolutions per day: | 14.45364568 |
mean anomaly at epoch: | 234.6548° |
orbit number at epoch: | 11370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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