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 25073.85652051 .00016840 00000-0 30216-3 0 9993
2 25544 51.6358 54.2440 0006407 21.9595 338.1668 15.50010161500535
| Epoch (UTC): | 14 March 2025 20:33:23 |
| Eccentricity: | 0.0006407 |
| inclination: | 51.6358° |
| perigee height: | 412 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 54.2440° |
| argument of perigee: | 21.9595° |
| revolutions per day: | 15.50010161 |
| mean anomaly at epoch: | 338.1668° |
| orbit number at epoch: | 50053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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