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 20480U 90013C 23088.56950410 -.00000013 00000-0 52855-4 0 9992
2 20480 99.0547 216.0429 0539291 287.8931 66.4083 12.83442310552525
| Epoch (UTC): | 29 March 2023 13:40:05 |
| Eccentricity: | 0.0539291 |
| inclination: | 99.0547° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 216.0429° |
| argument of perigee: | 287.8931° |
| revolutions per day: | 12.83442310 |
| mean anomaly at epoch: | 66.4083° |
| orbit number at epoch: | 55252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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