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 00561U 26101.40089411 +.00000000 +00000-0 +15283-2 0 00003
2 00561 67.7514 95.4509 0630306 343.5106 165.5936 12.41490723 04
| Epoch (UTC): | 11 April 2026 09:37:17 |
| Eccentricity: | 0.0630306 |
| inclination: | 67.7514° |
| perigee height: | 1004 km |
| apogee height: | 1997 km |
| right ascension of ascending node: | 95.4509° |
| argument of perigee: | 343.5106° |
| revolutions per day: | 12.41490723 |
| mean anomaly at epoch: | 165.5936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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