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 20443U 90005H 25189.46400786 .00000187 00000-0 73434-4 0 9998
2 20443 98.3451 251.8935 0009469 213.2398 146.8197 14.39651334857661
| Epoch (UTC): | 08 July 2025 11:08:10 |
| Eccentricity: | 0.0009469 |
| inclination: | 98.3451° |
| perigee height: | 753 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 251.8935° |
| argument of perigee: | 213.2398° |
| revolutions per day: | 14.39651334 |
| mean anomaly at epoch: | 146.8197° |
| orbit number at epoch: | 85766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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