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 35943U 26150.51560479 +.00000000 +00000-0 +00000-0 0 00008
2 35943 0.0441 69.0668 0003190 1.0968 66.5074 1.00270367 01
| Epoch (UTC): | 30 May 2026 12:22:28 |
| Eccentricity: | 0.0003190 |
| inclination: | 0.0441° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 69.0668° |
| argument of perigee: | 1.0968° |
| revolutions per day: | 1.00270367 |
| mean anomaly at epoch: | 66.5074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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