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 23153.54597696 -.00000006 00000-0 29380-4 0 9992
2 20478 99.3724 188.3941 0004956 334.8888 25.2031 13.95667234617088
| Epoch (UTC): | 02 June 2023 13:06:12 |
| Eccentricity: | 0.0004956 |
| inclination: | 99.3724° |
| perigee height: | 905 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 188.3941° |
| argument of perigee: | 334.8888° |
| revolutions per day: | 13.95667234 |
| mean anomaly at epoch: | 25.2031° |
| orbit number at epoch: | 61708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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