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 is defined by the following mean orbital elements,
1 37932U 26019.11905616 +.00000000 +00000-0 +82323-4 0 00006
2 37932 98.8708 333.3546 0036160 330.0069 40.6970 14.22966052 03
| Epoch (UTC): | 19 January 2026 02:51:26 |
| Eccentricity: | 0.0036160 |
| inclination: | 98.8708° |
| perigee height: | 789 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 333.3546° |
| argument of perigee: | 330.0069° |
| revolutions per day: | 14.22966052 |
| mean anomaly at epoch: | 40.6970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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