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 41384U 26145.59014178 +.00000000 +00000-0 +00000-0 0 00006
2 41384 5.2925 97.2937 0016875 187.4653 203.2896 1.00271458 01
| Epoch (UTC): | 25 May 2026 14:09:48 |
| Eccentricity: | 0.0016875 |
| inclination: | 5.2925° |
| perigee height: | 35716 km |
| apogee height: | 35858 km |
| right ascension of ascending node: | 97.2937° |
| argument of perigee: | 187.4653° |
| revolutions per day: | 1.00271458 |
| mean anomaly at epoch: | 203.2896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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