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 20438U 90005C 23082.80183044 .00000227 00000-0 10352-3 0 9999
2 20438 98.9249 99.0475 0009520 197.3679 336.1314 14.31211938731209
| Epoch (UTC): | 23 March 2023 19:14:38 |
| Eccentricity: | 0.0009520 |
| inclination: | 98.9249° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 99.0475° |
| argument of perigee: | 197.3679° |
| revolutions per day: | 14.31211938 |
| mean anomaly at epoch: | 336.1314° |
| orbit number at epoch: | 73120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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