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 44780U 26145.64805894 +.00000000 +00000-0 +69608-4 0 00001
2 44780 45.0090 280.9087 0006292 39.0823 321.0464 14.02053624 08
| Epoch (UTC): | 25 May 2026 15:33:12 |
| Eccentricity: | 0.0006292 |
| inclination: | 45.0090° |
| perigee height: | 882 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 280.9087° |
| argument of perigee: | 39.0823° |
| revolutions per day: | 14.02053624 |
| mean anomaly at epoch: | 321.0464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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