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 42747U 26145.59326182 +.00000000 +00000-0 +00000-0 0 00001
2 42747 0.0768 94.1963 0007014 336.2014 74.2368 1.00271276 06
| Epoch (UTC): | 25 May 2026 14:14:17 |
| Eccentricity: | 0.0007014 |
| inclination: | 0.0768° |
| perigee height: | 35757 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 94.1963° |
| argument of perigee: | 336.2014° |
| revolutions per day: | 1.00271276 |
| mean anomaly at epoch: | 74.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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