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 44927U 26145.57661267 +.00000000 +00000-0 +92642-3 0 00003
2 44927 53.0420 316.4804 0001412 343.1482 16.9485 15.63280570 01
| Epoch (UTC): | 25 May 2026 13:50:19 |
| Eccentricity: | 0.0001412 |
| inclination: | 53.0420° |
| perigee height: | 377 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 316.4804° |
| argument of perigee: | 343.1482° |
| revolutions per day: | 15.63280570 |
| mean anomaly at epoch: | 16.9485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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