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 14781U 84021B 24252.86847419 .00006107 00000-0 68198-3 0 9997
2 14781 97.7143 219.6920 0008921 149.3647 210.8092 14.87306448181925
Epoch (UTC): | 08 September 2024 20:50:36 |
Eccentricity: | 0.0008921 |
inclination: | 97.7143° |
perigee height: | 600 km |
apogee height: | 612 km |
right ascension of ascending node: | 219.6920° |
argument of perigee: | 149.3647° |
revolutions per day: | 14.87306448 |
mean anomaly at epoch: | 210.8092° |
orbit number at epoch: | 18192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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