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 26160.73324714 +.00000000 +00000-0 +53342-3 0 00001
2 25979 98.1602 252.3278 0004867 124.8873 235.2826 15.34662230 07
| Epoch (UTC): | 09 June 2026 17:35:52 |
| Eccentricity: | 0.0004867 |
| inclination: | 98.1602° |
| perigee height: | 459 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 252.3278° |
| argument of perigee: | 124.8873° |
| revolutions per day: | 15.34662230 |
| mean anomaly at epoch: | 235.2826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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