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 26140.12358490 +.00000000 +00000-0 +00000-0 0 00007
2 41879 0.0058 4.7991 0000219 358.8472 68.4241 1.00271234 08
| Epoch (UTC): | 20 May 2026 02:57:57 |
| Eccentricity: | 0.0000219 |
| inclination: | 0.0058° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 4.7991° |
| argument of perigee: | 358.8472° |
| revolutions per day: | 1.00271234 |
| mean anomaly at epoch: | 68.4241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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