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 43477U 18047B 26065.62856469 +.00005555 00000-0 +15106-3 0 09
2 43477 88.9903 212.0354 0013065 141.7389 321.5579 15.37396437434044
| Epoch (UTC): | 06 March 2026 15:05:07 |
| Eccentricity: | 0.0013065 |
| inclination: | 88.9903° |
| perigee height: | 445 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 212.0354° |
| argument of perigee: | 141.7389° |
| revolutions per day: | 15.37396437 |
| mean anomaly at epoch: | 321.5579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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