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 20453U 90008B 23027.27321298 .00015417 00000-0 76009-3 0 9992
2 20453 35.6240 12.1326 0252147 15.0328 345.7718 14.93520229753334
| Epoch (UTC): | 27 January 2023 06:33:25 |
| Eccentricity: | 0.0252147 |
| inclination: | 35.6240° |
| perigee height: | 411 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 12.1326° |
| argument of perigee: | 15.0328° |
| revolutions per day: | 14.93520229 |
| mean anomaly at epoch: | 345.7718° |
| orbit number at epoch: | 75333 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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