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 61020U 26145.53965100 +.00000000 +00000-0 +17790-3 0 00006
2 61020 49.9983 188.2650 0003825 16.1080 343.9980 14.84137792 09
| Epoch (UTC): | 25 May 2026 12:57:05 |
| Eccentricity: | 0.0003825 |
| inclination: | 49.9983° |
| perigee height: | 614 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 188.2650° |
| argument of perigee: | 16.1080° |
| revolutions per day: | 14.84137792 |
| mean anomaly at epoch: | 343.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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