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 24292U 96050B 25130.55459719 -.00000038 00000-0 28526-3 0 9993
2 24292 62.7442 310.7347 5636171 262.2117 33.7711 4.14728162434526
Epoch (UTC): | 10 May 2025 13:18:37 |
Eccentricity: | 0.5636171 |
inclination: | 62.7442° |
perigee height: | 763 km |
apogee height: | 19209 km |
right ascension of ascending node: | 310.7347° |
argument of perigee: | 262.2117° |
revolutions per day: | 4.14728162 |
mean anomaly at epoch: | 33.7711° |
orbit number at epoch: | 43452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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