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 61755U 26145.51365698 +.00000000 +00000-0 +71752-3 0 00003
2 61755 97.2948 23.9616 0003539 29.0608 331.0848 15.65051341 05
| Epoch (UTC): | 25 May 2026 12:19:39 |
| Eccentricity: | 0.0003539 |
| inclination: | 97.2948° |
| perigee height: | 371 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 23.9616° |
| argument of perigee: | 29.0608° |
| revolutions per day: | 15.65051341 |
| mean anomaly at epoch: | 331.0848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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