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 61950U 26145.57524765 +.00000000 +00000-0 +14393-2 0 00005
2 61950 53.1568 352.2464 0000677 89.5861 270.5235 15.69802796 01
| Epoch (UTC): | 25 May 2026 13:48:21 |
| Eccentricity: | 0.0000677 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 352.2464° |
| argument of perigee: | 89.5861° |
| revolutions per day: | 15.69802796 |
| mean anomaly at epoch: | 270.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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