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 25979U 26162.49367458 +.00000000 +00000-0 +50740-3 0 00007
2 25979 98.1608 254.2742 0004833 119.8773 240.2948 15.34722722 00
| Epoch (UTC): | 11 June 2026 11:50:53 |
| Eccentricity: | 0.0004833 |
| inclination: | 98.1608° |
| perigee height: | 458 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 254.2742° |
| argument of perigee: | 119.8773° |
| revolutions per day: | 15.34722722 |
| mean anomaly at epoch: | 240.2948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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