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 40294U 26144.98987678 +.00000000 +00000-0 +00000-0 0 00001
2 40294 56.9722 31.8484 0066401 69.7589 290.9872 2.00574806 00
| Epoch (UTC): | 24 May 2026 23:45:25 |
| Eccentricity: | 0.0066401 |
| inclination: | 56.9722° |
| perigee height: | 20005 km |
| apogee height: | 20358 km |
| right ascension of ascending node: | 31.8484° |
| argument of perigee: | 69.7589° |
| revolutions per day: | 2.00574806 |
| mean anomaly at epoch: | 290.9872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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