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 43784U 26050.09818235 +.00000000 +00000-0 +45103-3 0 00004
2 43784 97.4046 105.6790 0002706 16.2486 343.8838 15.24291111 02
| Epoch (UTC): | 19 February 2026 02:21:22 |
| Eccentricity: | 0.0002706 |
| inclination: | 97.4046° |
| perigee height: | 491 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 105.6790° |
| argument of perigee: | 16.2486° |
| revolutions per day: | 15.24291111 |
| mean anomaly at epoch: | 343.8838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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