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 43476U 18047A 26064.58689804 +.00004724 00000-0 +12851-3 0 00
2 43476 88.9903 212.1789 0012962 145.2930 318.3319 15.37387408433887
| Epoch (UTC): | 05 March 2026 14:05:07 |
| Eccentricity: | 0.0012962 |
| inclination: | 88.9903° |
| perigee height: | 445 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 212.1789° |
| argument of perigee: | 145.2930° |
| revolutions per day: | 15.37387408 |
| mean anomaly at epoch: | 318.3319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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