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 20442U 90005G 25118.93901051 .00000333 00000-0 13610-3 0 9994
2 20442 98.8995 123.9464 0011230 346.2329 13.8547 14.33935817843026
| Epoch (UTC): | 28 April 2025 22:32:10 |
| Eccentricity: | 0.0011230 |
| inclination: | 98.8995° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 123.9464° |
| argument of perigee: | 346.2329° |
| revolutions per day: | 14.33935817 |
| mean anomaly at epoch: | 13.8547° |
| orbit number at epoch: | 84302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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