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 61786U 26145.63513594 +.00000000 +00000-0 +57055-3 0 00000
2 61786 97.2982 19.6449 0009917 26.6400 333.5358 15.47495827 06
| Epoch (UTC): | 25 May 2026 15:14:35 |
| Eccentricity: | 0.0009917 |
| inclination: | 97.2982° |
| perigee height: | 417 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 19.6449° |
| argument of perigee: | 26.6400° |
| revolutions per day: | 15.47495827 |
| mean anomaly at epoch: | 333.5358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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