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 61785U 26145.63045596 +.00000000 +00000-0 +67729-3 0 00000
2 61785 97.2979 21.7422 0008177 18.2640 341.8908 15.58404222 00
| Epoch (UTC): | 25 May 2026 15:07:51 |
| Eccentricity: | 0.0008177 |
| inclination: | 97.2979° |
| perigee height: | 387 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 21.7422° |
| argument of perigee: | 18.2640° |
| revolutions per day: | 15.58404222 |
| mean anomaly at epoch: | 341.8908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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