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 61979U 26145.26621032 +.00000000 +00000-0 +57113-3 0 00005
2 61979 43.0007 107.1630 0001211 273.6270 86.4443 15.27594826 06
| Epoch (UTC): | 25 May 2026 06:23:20 |
| Eccentricity: | 0.0001211 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.1630° |
| argument of perigee: | 273.6270° |
| revolutions per day: | 15.27594826 |
| mean anomaly at epoch: | 86.4443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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