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 26108.12268517 +.00002558 00000-0 +68674-4 0 02
2 43477 88.9953 206.1985 0009801 1.0534 82.5532 15.37839166440575
| Epoch (UTC): | 18 April 2026 02:56:39 |
| Eccentricity: | 0.0009801 |
| inclination: | 88.9953° |
| perigee height: | 446 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 206.1985° |
| argument of perigee: | 1.0534° |
| revolutions per day: | 15.37839166 |
| mean anomaly at epoch: | 82.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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