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 41879U 26146.21711273 +.00000000 +00000-0 +00000-0 0 00005
2 41879 0.0052 352.2527 0000227 3.3971 116.1087 1.00272560 05
| Epoch (UTC): | 26 May 2026 05:12:38 |
| Eccentricity: | 0.0000227 |
| inclination: | 0.0052° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 352.2527° |
| argument of perigee: | 3.3971° |
| revolutions per day: | 1.00272560 |
| mean anomaly at epoch: | 116.1087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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