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 00022U 59009A 25346.97737041 .00016137 00000-0 60860-3 0 9996
2 00022 50.2555 297.7443 0085819 95.1959 265.8800 15.23751528771905
| Epoch (UTC): | 12 December 2025 23:27:24 |
| Eccentricity: | 0.0085819 |
| inclination: | 50.2555° |
| perigee height: | 435 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 297.7443° |
| argument of perigee: | 95.1959° |
| revolutions per day: | 15.23751528 |
| mean anomaly at epoch: | 265.8800° |
| orbit number at epoch: | 77190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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