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 44781U 26145.63245605 +.00000000 +00000-0 +28089-4 0 00007
2 44781 45.0001 279.1915 0009329 38.0323 322.1168 14.02049229 08
| Epoch (UTC): | 25 May 2026 15:10:44 |
| Eccentricity: | 0.0009329 |
| inclination: | 45.0001° |
| perigee height: | 880 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 279.1915° |
| argument of perigee: | 38.0323° |
| revolutions per day: | 14.02049229 |
| mean anomaly at epoch: | 322.1168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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