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 43565U 26141.88833609 +.00000000 +00000-0 +00000-0 0 00005
2 43565 57.1815 342.4938 0001850 271.2445 88.7537 1.70475538 02
| Epoch (UTC): | 21 May 2026 21:19:12 |
| Eccentricity: | 0.0001850 |
| inclination: | 57.1815° |
| perigee height: | 23217 km |
| apogee height: | 23227 km |
| right ascension of ascending node: | 342.4938° |
| argument of perigee: | 271.2445° |
| revolutions per day: | 1.70475538 |
| mean anomaly at epoch: | 88.7537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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