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 66868U 26144.80999022 +.00000000 +00000-0 +69953-3 0 00008
2 66868 43.0019 273.8931 0001604 276.6550 83.4119 15.27595883 07
| Epoch (UTC): | 24 May 2026 19:26:23 |
| Eccentricity: | 0.0001604 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.8931° |
| argument of perigee: | 276.6550° |
| revolutions per day: | 15.27595883 |
| mean anomaly at epoch: | 83.4119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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