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 35686U 26134.19179075 +.00000000 +00000-0 +72200-4 0 00001
2 35686 98.2026 285.7990 0061727 178.1571 181.9888 14.96125410 06
| Epoch (UTC): | 14 May 2026 04:36:10 |
| Eccentricity: | 0.0061727 |
| inclination: | 98.2026° |
| perigee height: | 536 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 285.7990° |
| argument of perigee: | 178.1571° |
| revolutions per day: | 14.96125410 |
| mean anomaly at epoch: | 181.9888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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