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 42965U 26144.39920994 +.00000000 +00000-0 +00000-0 0 00001
2 42965 40.1220 343.7839 0745359 271.4032 269.2555 1.00258100 07
| Epoch (UTC): | 24 May 2026 09:34:51 |
| Eccentricity: | 0.0745359 |
| inclination: | 40.1220° |
| perigee height: | 32647 km |
| apogee height: | 38934 km |
| right ascension of ascending node: | 343.7839° |
| argument of perigee: | 271.4032° |
| revolutions per day: | 1.00258100 |
| mean anomaly at epoch: | 269.2555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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