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 26065.10356470 +.00005307 00000-0 +14435-3 0 08
2 43477 88.9902 212.1079 0013019 143.4495 296.2279 15.37389595433966
| Epoch (UTC): | 06 March 2026 02:29:07 |
| Eccentricity: | 0.0013019 |
| inclination: | 88.9902° |
| perigee height: | 445 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 212.1079° |
| argument of perigee: | 143.4495° |
| revolutions per day: | 15.37389595 |
| mean anomaly at epoch: | 296.2279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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