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 43180U 26150.53528337 +.00000000 +00000-0 +15552-3 0 00000
2 43180 97.3601 56.4149 0001876 80.6329 279.5120 15.22893180 08
| Epoch (UTC): | 30 May 2026 12:50:48 |
| Eccentricity: | 0.0001876 |
| inclination: | 97.3601° |
| perigee height: | 496 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 56.4149° |
| argument of perigee: | 80.6329° |
| revolutions per day: | 15.22893180 |
| mean anomaly at epoch: | 279.5120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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