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 45381C 20019X 23336.13173611 -.00033882 00000+0 -22738-2 0 3367
2 45381 53.0535 266.1616 0001650 69.2101 191.6869 15.06372574 14
| Epoch (UTC): | 02 December 2023 03:09:42 |
| Eccentricity: | 0.0001650 |
| inclination: | 53.0535° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 266.1616° |
| argument of perigee: | 69.2101° |
| revolutions per day: | 15.06372574 |
| mean anomaly at epoch: | 191.6869° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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