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 56036U 26145.51636534 +.00000000 +00000-0 +12106-4 0 00008
2 56036 43.0042 331.4553 0002237 257.3973 102.6629 15.27589860 06
| Epoch (UTC): | 25 May 2026 12:23:33 |
| Eccentricity: | 0.0002237 |
| inclination: | 43.0042° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 331.4553° |
| argument of perigee: | 257.3973° |
| revolutions per day: | 15.27589860 |
| mean anomaly at epoch: | 102.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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