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 61859U 26145.49360963 +.00000000 +00000-0 +75343-4 0 00006
2 61859 43.0025 164.2550 0001198 289.6946 70.3776 15.27592292 05
| Epoch (UTC): | 25 May 2026 11:50:47 |
| Eccentricity: | 0.0001198 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.2550° |
| argument of perigee: | 289.6946° |
| revolutions per day: | 15.27592292 |
| mean anomaly at epoch: | 70.3776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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