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 25544U 98067A 23271.18340520 .00029694 00000-0 52925-3 0 9994
2 25544 51.6417 178.3702 0005768 66.3129 85.7053 15.49829609417763
| Epoch (UTC): | 28 September 2023 04:24:06 |
| Eccentricity: | 0.0005768 |
| inclination: | 51.6417° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 178.3702° |
| argument of perigee: | 66.3129° |
| revolutions per day: | 15.49829609 |
| mean anomaly at epoch: | 85.7053° |
| orbit number at epoch: | 41776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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