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 57967U 26145.35696220 +.00000000 +00000-0 +37958-4 0 00004
2 57967 43.0034 262.8585 0001388 272.5360 87.5333 15.27581392 03
| Epoch (UTC): | 25 May 2026 08:34:01 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.8585° |
| argument of perigee: | 272.5360° |
| revolutions per day: | 15.27581392 |
| mean anomaly at epoch: | 87.5333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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