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 43789U 18099AH 25341.15040997 .00154627 00000-0 17901-2 0 9993
2 43789 97.4407 54.1147 0005532 208.5963 151.4992 15.61310389384906
| Epoch (UTC): | 07 December 2025 03:36:35 |
| Eccentricity: | 0.0005532 |
| inclination: | 97.4407° |
| perigee height: | 380 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 54.1147° |
| argument of perigee: | 208.5963° |
| revolutions per day: | 15.61310389 |
| mean anomaly at epoch: | 151.4992° |
| orbit number at epoch: | 38490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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