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 61594U 26145.42043830 +.00000000 +00000-0 +14029-2 0 00008
2 61594 87.8907 25.6230 0002345 84.9325 275.2070 13.11416943 05
| Epoch (UTC): | 25 May 2026 10:05:25 |
| Eccentricity: | 0.0002345 |
| inclination: | 87.8907° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6230° |
| argument of perigee: | 84.9325° |
| revolutions per day: | 13.11416943 |
| mean anomaly at epoch: | 275.2070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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