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 44606U 16068F 25341.01193452 .00000684 00000-0 45498-3 0 9992
2 44606 98.4426 69.8309 0223922 20.2830 340.7056 13.92734139459684
| Epoch (UTC): | 07 December 2025 00:17:11 |
| Eccentricity: | 0.0223922 |
| inclination: | 98.4426° |
| perigee height: | 755 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 69.8309° |
| argument of perigee: | 20.2830° |
| revolutions per day: | 13.92734139 |
| mean anomaly at epoch: | 340.7056° |
| orbit number at epoch: | 45968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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