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 43539U 26144.96425000 +.00000000 +00000-0 +00000-0 0 00000
2 43539 55.1903 163.2595 0104267 237.9351 300.0258 1.00257887 06
| Epoch (UTC): | 24 May 2026 23:08:31 |
| Eccentricity: | 0.0104267 |
| inclination: | 55.1903° |
| perigee height: | 35351 km |
| apogee height: | 36230 km |
| right ascension of ascending node: | 163.2595° |
| argument of perigee: | 237.9351° |
| revolutions per day: | 1.00257887 |
| mean anomaly at epoch: | 300.0258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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