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 43779U 26087.84820296 +.00000000 +00000-0 +21248-3 0 00005
2 43779 97.4496 133.4135 0011611 314.4126 45.6151 15.07185466 07
| Epoch (UTC): | 28 March 2026 20:21:24 |
| Eccentricity: | 0.0011611 |
| inclination: | 97.4496° |
| perigee height: | 537 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 133.4135° |
| argument of perigee: | 314.4126° |
| revolutions per day: | 15.07185466 |
| mean anomaly at epoch: | 45.6151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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