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 53807U 22111AL 24251.08079763 .00017944 00000-0 66050-3 0 9999
2 53807 53.2345 175.8051 0007631 0.1569 359.9433 15.27923094110743
| Epoch (UTC): | 07 September 2024 01:56:20 |
| Eccentricity: | 0.0007631 |
| inclination: | 53.2345° |
| perigee height: | 477 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 175.8051° |
| argument of perigee: | 0.1569° |
| revolutions per day: | 15.27923094 |
| mean anomaly at epoch: | 359.9433° |
| orbit number at epoch: | 11074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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