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 41826U 99025EYD 25348.63119379 .00003245 00000-0 14157-2 0 9991
2 41826 98.7337 54.4126 0055945 218.1800 141.5410 14.23763701473879
| Epoch (UTC): | 14 December 2025 15:08:55 |
| Eccentricity: | 0.0055945 |
| inclination: | 98.7337° |
| perigee height: | 772 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 54.4126° |
| argument of perigee: | 218.1800° |
| revolutions per day: | 14.23763701 |
| mean anomaly at epoch: | 141.5410° |
| orbit number at epoch: | 47387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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