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 25138.73669831 .00013314 00000-0 61434-3 0 9990
2 43803 97.4668 198.0150 0007077 208.3607 151.7243 15.20335835353459
| Epoch (UTC): | 18 May 2025 17:40:50 |
| Eccentricity: | 0.0007077 |
| inclination: | 97.4668° |
| perigee height: | 500 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 198.0150° |
| argument of perigee: | 208.3607° |
| revolutions per day: | 15.20335835 |
| mean anomaly at epoch: | 151.7243° |
| orbit number at epoch: | 35345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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