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 47787U 26145.00355867 +.00000000 +00000-0 -45005-4 0 00007
2 47787 53.1621 250.7593 0000431 228.0184 132.0780 15.31704448 05
| Epoch (UTC): | 25 May 2026 00:05:07 |
| Eccentricity: | 0.0000431 |
| inclination: | 53.1621° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 250.7593° |
| argument of perigee: | 228.0184° |
| revolutions per day: | 15.31704448 |
| mean anomaly at epoch: | 132.0780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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