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 32260U 26144.79071294 +.00000000 +00000-0 +00000-0 0 00002
2 32260 54.0788 81.0295 0165818 86.9308 274.9410 2.00556397 09
| Epoch (UTC): | 24 May 2026 18:58:37 |
| Eccentricity: | 0.0165818 |
| inclination: | 54.0788° |
| perigee height: | 19742 km |
| apogee height: | 20623 km |
| right ascension of ascending node: | 81.0295° |
| argument of perigee: | 86.9308° |
| revolutions per day: | 2.00556397 |
| mean anomaly at epoch: | 274.9410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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