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 61924U 26145.49161506 +.00000000 +00000-0 +54927-3 0 00005
2 61924 43.0024 211.8327 0001809 270.8329 89.2315 15.27591808 04
| Epoch (UTC): | 25 May 2026 11:47:55 |
| Eccentricity: | 0.0001809 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.8327° |
| argument of perigee: | 270.8329° |
| revolutions per day: | 15.27591808 |
| mean anomaly at epoch: | 89.2315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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