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 66861U 26144.63424409 +.00000000 +00000-0 +74127-3 0 00003
2 66861 43.0004 274.2884 0000515 243.1788 116.9011 15.27593664 06
| Epoch (UTC): | 24 May 2026 15:13:18 |
| Eccentricity: | 0.0000515 |
| inclination: | 43.0004° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 274.2884° |
| argument of perigee: | 243.1788° |
| revolutions per day: | 15.27593664 |
| mean anomaly at epoch: | 116.9011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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