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 43480U 26145.36363689 +.00000000 +00000-0 +11906-4 0 00005
2 43480 86.3946 97.8792 0002185 84.2712 275.8733 14.34217885 07
| Epoch (UTC): | 25 May 2026 08:43:38 |
| Eccentricity: | 0.0002185 |
| inclination: | 86.3946° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.8792° |
| argument of perigee: | 84.2712° |
| revolutions per day: | 14.34217885 |
| mean anomaly at epoch: | 275.8733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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