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 56786U 26145.40691064 +.00000000 +00000-0 -14639-4 0 00001
2 56786 69.9989 131.0811 0003620 266.7523 93.3222 14.98331097 07
| Epoch (UTC): | 25 May 2026 09:45:57 |
| Eccentricity: | 0.0003620 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.0811° |
| argument of perigee: | 266.7523° |
| revolutions per day: | 14.98331097 |
| mean anomaly at epoch: | 93.3222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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