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 43564U 26141.08213772 +.00000000 +00000-0 +00000-0 0 00009
2 43564 57.1776 342.5120 0003144 316.0402 43.9551 1.70475772 09
| Epoch (UTC): | 21 May 2026 01:58:16 |
| Eccentricity: | 0.0003144 |
| inclination: | 57.1776° |
| perigee height: | 23213 km |
| apogee height: | 23231 km |
| right ascension of ascending node: | 342.5120° |
| argument of perigee: | 316.0402° |
| revolutions per day: | 1.70475772 |
| mean anomaly at epoch: | 43.9551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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