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 43803U 18099AX 23334.13497160 .00011395 00000-0 84159-3 0 9990
2 43803 97.5482 32.5697 0009753 264.9834 95.0278 15.03362191272606
| Epoch (UTC): | 30 November 2023 03:14:21 |
| Eccentricity: | 0.0009753 |
| inclination: | 97.5482° |
| perigee height: | 550 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 32.5697° |
| argument of perigee: | 264.9834° |
| revolutions per day: | 15.03362191 |
| mean anomaly at epoch: | 95.0278° |
| orbit number at epoch: | 27260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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