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 28480U 04046B 22221.38350812 .00000088 00000-0 47706-4 0 9999
2 28480 98.0677 204.9705 0142939 65.6672 295.9359 14.25845507921980
| Epoch (UTC): | 09 August 2022 09:12:15 |
| Eccentricity: | 0.0142939 |
| inclination: | 98.0677° |
| perigee height: | 703 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 204.9705° |
| argument of perigee: | 65.6672° |
| revolutions per day: | 14.25845507 |
| mean anomaly at epoch: | 295.9359° |
| orbit number at epoch: | 92198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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