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 56483U 26145.41710719 +.00000000 +00000-0 +90541-4 0 00000
2 56483 69.9985 290.9379 0002770 269.6881 90.3961 14.98319634 05
| Epoch (UTC): | 25 May 2026 10:00:38 |
| Eccentricity: | 0.0002770 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.9379° |
| argument of perigee: | 269.6881° |
| revolutions per day: | 14.98319634 |
| mean anomaly at epoch: | 90.3961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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