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 56169U 26145.33957493 +.00000000 +00000-0 +20781-4 0 00003
2 56169 81.0019 93.3277 0007709 23.4874 336.6633 13.85146540 07
| Epoch (UTC): | 25 May 2026 08:08:59 |
| Eccentricity: | 0.0007709 |
| inclination: | 81.0019° |
| perigee height: | 940 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 93.3277° |
| argument of perigee: | 23.4874° |
| revolutions per day: | 13.85146540 |
| mean anomaly at epoch: | 336.6633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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