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 26150.79783792 +.00000000 +00000-0 +25277-3 0 00002
2 35685 98.1147 268.9410 0048671 220.4730 139.2865 14.93002426 08
| Epoch (UTC): | 30 May 2026 19:08:53 |
| Eccentricity: | 0.0048671 |
| inclination: | 98.1147° |
| perigee height: | 555 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 268.9410° |
| argument of perigee: | 220.4730° |
| revolutions per day: | 14.93002426 |
| mean anomaly at epoch: | 139.2865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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