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 20478U 90013A 23150.10490772 .00000205 00000-0 18431-3 0 9992
2 20478 99.3726 184.8945 0005112 345.6732 14.4284 13.95666157616811
| Epoch (UTC): | 30 May 2023 02:31:04 |
| Eccentricity: | 0.0005112 |
| inclination: | 99.3726° |
| perigee height: | 905 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 184.8945° |
| argument of perigee: | 345.6732° |
| revolutions per day: | 13.95666157 |
| mean anomaly at epoch: | 14.4284° |
| orbit number at epoch: | 61681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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