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 20046U 89042B 25198.26556212 .00000076 00000-0 59192-4 0 9992
2 20046 82.9354 262.4866 0043250 69.5683 291.0111 13.78567816815696
| Epoch (UTC): | 17 July 2025 06:22:24 |
| Eccentricity: | 0.0043250 |
| inclination: | 82.9354° |
| perigee height: | 937 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 262.4866° |
| argument of perigee: | 69.5683° |
| revolutions per day: | 13.78567816 |
| mean anomaly at epoch: | 291.0111° |
| orbit number at epoch: | 81569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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