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 25139.18441541 .00007929 00000-0 14879-3 0 9997
2 25544 51.6355 90.7571 0002193 124.9576 235.1619 15.49604105510665
| Epoch (UTC): | 19 May 2025 04:25:33 |
| Eccentricity: | 0.0002193 |
| inclination: | 51.6355° |
| perigee height: | 416 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 90.7571° |
| argument of perigee: | 124.9576° |
| revolutions per day: | 15.49604105 |
| mean anomaly at epoch: | 235.1619° |
| orbit number at epoch: | 51066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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