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 61935U 26145.21465154 +.00000000 +00000-0 +46974-3 0 00006
2 61935 42.9943 213.1908 0000765 299.6317 60.4458 15.27587746 05
| Epoch (UTC): | 25 May 2026 05:09:05 |
| Eccentricity: | 0.0000765 |
| inclination: | 42.9943° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 213.1908° |
| argument of perigee: | 299.6317° |
| revolutions per day: | 15.27587746 |
| mean anomaly at epoch: | 60.4458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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