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 61966U 26145.54497411 +.00000000 +00000-0 +83581-3 0 00002
2 61966 42.9951 91.1077 0001126 61.5590 298.5375 15.27576856 02
| Epoch (UTC): | 25 May 2026 13:04:45 |
| Eccentricity: | 0.0001126 |
| inclination: | 42.9951° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 91.1077° |
| argument of perigee: | 61.5590° |
| revolutions per day: | 15.27576856 |
| mean anomaly at epoch: | 298.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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