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 25136.49952537 .00000169 00000-0 15164-3 0 9992
2 20046 82.9345 308.5652 0040736 241.0334 118.6737 13.78556883807182
| Epoch (UTC): | 16 May 2025 11:59:18 |
| Eccentricity: | 0.0040736 |
| inclination: | 82.9345° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 308.5652° |
| argument of perigee: | 241.0334° |
| revolutions per day: | 13.78556883 |
| mean anomaly at epoch: | 118.6737° |
| orbit number at epoch: | 80718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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