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 61872U 26144.81812822 +.00000000 +00000-0 +43311-3 0 00001
2 61872 97.4263 215.0779 0012255 70.0626 290.1931 15.26705251 03
| Epoch (UTC): | 24 May 2026 19:38:06 |
| Eccentricity: | 0.0012255 |
| inclination: | 97.4263° |
| perigee height: | 477 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 215.0779° |
| argument of perigee: | 70.0626° |
| revolutions per day: | 15.26705251 |
| mean anomaly at epoch: | 290.1931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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