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 43678U 18084H 25348.32038787 .00003977 00000-0 32952-3 0 9999
2 43678 98.1027 171.8465 0007641 42.5647 317.6166 14.99447391388500
| Epoch (UTC): | 14 December 2025 07:41:21 |
| Eccentricity: | 0.0007641 |
| inclination: | 98.1027° |
| perigee height: | 563 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 171.8465° |
| argument of perigee: | 42.5647° |
| revolutions per day: | 14.99447391 |
| mean anomaly at epoch: | 317.6166° |
| orbit number at epoch: | 38850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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