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 43272U 26145.43454676 +.00000000 +00000-0 +00000-0 0 00008
2 43272 0.0524 99.7095 0001227 329.9689 296.2583 1.00273709 02
| Epoch (UTC): | 25 May 2026 10:25:44 |
| Eccentricity: | 0.0001227 |
| inclination: | 0.0524° |
| perigee height: | 35781 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 99.7095° |
| argument of perigee: | 329.9689° |
| revolutions per day: | 1.00273709 |
| mean anomaly at epoch: | 296.2583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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