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 44881U 19093C 25311.28278591 .00001641 00000-0 19368-3 0 9993
2 44881 97.7796 23.7029 0015125 96.3182 263.9756 14.85976792318455
| Epoch (UTC): | 07 November 2025 06:47:12 |
| Eccentricity: | 0.0015125 |
| inclination: | 97.7796° |
| perigee height: | 600 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 23.7029° |
| argument of perigee: | 96.3182° |
| revolutions per day: | 14.85976792 |
| mean anomaly at epoch: | 263.9756° |
| orbit number at epoch: | 31845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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