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 4615U 70025T 24357.85526262 .00000451 00000-0 54093-3 0 9991
2 4615 100.1184 85.9415 0059668 48.8718 62.7995 13.72363024728843
| Epoch (UTC): | 22 December 2024 20:31:34 |
| Eccentricity: | 0.0059668 |
| inclination: | 100.1184° |
| perigee height: | 947 km |
| apogee height: | 1035 km |
| right ascension of ascending node: | 85.9415° |
| argument of perigee: | 48.8718° |
| revolutions per day: | 13.72363024 |
| mean anomaly at epoch: | 62.7995° |
| orbit number at epoch: | 72884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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