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 61928U 26145.52921791 +.00000000 +00000-0 +40888-3 0 00004
2 61928 43.0023 207.7929 0001419 271.3346 88.7343 15.27590381 01
| Epoch (UTC): | 25 May 2026 12:42:04 |
| Eccentricity: | 0.0001419 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.7929° |
| argument of perigee: | 271.3346° |
| revolutions per day: | 15.27590381 |
| mean anomaly at epoch: | 88.7343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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