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 35685U 26145.57019935 +.00000000 +00000-0 +11346-3 0 00005
2 35685 98.1141 263.5508 0048365 238.0946 121.5563 14.92980571 09
| Epoch (UTC): | 25 May 2026 13:41:05 |
| Eccentricity: | 0.0048365 |
| inclination: | 98.1141° |
| perigee height: | 555 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 263.5508° |
| argument of perigee: | 238.0946° |
| revolutions per day: | 14.92980571 |
| mean anomaly at epoch: | 121.5563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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