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 56689U 26145.53890705 +.00000000 +00000-0 +28570-4 0 00008
2 56689 42.9998 207.2030 0001323 272.8101 87.2599 15.26744122 05
| Epoch (UTC): | 25 May 2026 12:56:01 |
| Eccentricity: | 0.0001323 |
| inclination: | 42.9998° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 207.2030° |
| argument of perigee: | 272.8101° |
| revolutions per day: | 15.26744122 |
| mean anomaly at epoch: | 87.2599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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