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 41400U 00055KD 25080.48199006 .00011982 00000-0 45821-2 0 9994
2 41400 98.7198 170.6542 0020022 148.3902 211.8487 14.30687647467667
| Epoch (UTC): | 21 March 2025 11:34:03 |
| Eccentricity: | 0.0020022 |
| inclination: | 98.7198° |
| perigee height: | 775 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 170.6542° |
| argument of perigee: | 148.3902° |
| revolutions per day: | 14.30687647 |
| mean anomaly at epoch: | 211.8487° |
| orbit number at epoch: | 46766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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