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 61945U 26145.58996286 +.00000000 +00000-0 +15894-2 0 00008
2 61945 53.1574 352.3430 0000632 84.2586 275.8504 15.69812140 04
| Epoch (UTC): | 25 May 2026 14:09:32 |
| Eccentricity: | 0.0000632 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 352.3430° |
| argument of perigee: | 84.2586° |
| revolutions per day: | 15.69812140 |
| mean anomaly at epoch: | 275.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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