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 25193.91210898 .00000189 00000-0 74082-4 0 9998
2 20443 98.3448 256.2265 0009749 199.3669 160.7150 14.39653523858306
| Epoch (UTC): | 12 July 2025 21:53:26 |
| Eccentricity: | 0.0009749 |
| inclination: | 98.3448° |
| perigee height: | 752 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 256.2265° |
| argument of perigee: | 199.3669° |
| revolutions per day: | 14.39653523 |
| mean anomaly at epoch: | 160.7150° |
| orbit number at epoch: | 85830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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