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 56962U 26145.52094580 +.00000000 +00000-0 +57678-3 0 00008
2 56962 97.5930 306.7298 0003633 258.3182 101.7684 15.92390359 05
| Epoch (UTC): | 25 May 2026 12:30:09 |
| Eccentricity: | 0.0003633 |
| inclination: | 97.5930° |
| perigee height: | 293 km |
| apogee height: | 298 km |
| right ascension of ascending node: | 306.7298° |
| argument of perigee: | 258.3182° |
| revolutions per day: | 15.92390359 |
| mean anomaly at epoch: | 101.7684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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