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 44779U 26145.59282050 +.00000000 +00000-0 +27584-4 0 00003
2 44779 45.0061 280.8219 0010385 49.5011 310.6727 14.02036316 08
| Epoch (UTC): | 25 May 2026 14:13:39 |
| Eccentricity: | 0.0010385 |
| inclination: | 45.0061° |
| perigee height: | 879 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 280.8219° |
| argument of perigee: | 49.5011° |
| revolutions per day: | 14.02036316 |
| mean anomaly at epoch: | 310.6727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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