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 61946U 26145.58505750 +.00000000 +00000-0 +16249-2 0 00006
2 61946 53.1570 352.3067 0000979 113.8995 246.2126 15.69814371 04
| Epoch (UTC): | 25 May 2026 14:02:28 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 352.3067° |
| argument of perigee: | 113.8995° |
| revolutions per day: | 15.69814371 |
| mean anomaly at epoch: | 246.2126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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