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 43770U 26050.12901366 +.00000000 +00000-0 +41969-3 0 00007
2 43770 97.4549 110.9579 0010024 50.8708 309.3419 15.23879362 03
| Epoch (UTC): | 19 February 2026 03:05:46 |
| Eccentricity: | 0.0010024 |
| inclination: | 97.4549° |
| perigee height: | 487 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 110.9579° |
| argument of perigee: | 50.8708° |
| revolutions per day: | 15.23879362 |
| mean anomaly at epoch: | 309.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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