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 61856U 26145.48333458 +.00000000 +00000-0 +31291-4 0 00005
2 61856 43.0014 164.1767 0001299 276.7211 83.3493 15.27582309 01
| Epoch (UTC): | 25 May 2026 11:36:00 |
| Eccentricity: | 0.0001299 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.1767° |
| argument of perigee: | 276.7211° |
| revolutions per day: | 15.27582309 |
| mean anomaly at epoch: | 83.3493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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