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 56782U 26145.35267344 +.00000000 +00000-0 +24154-4 0 00003
2 56782 69.9987 131.2933 0003154 269.7394 90.3404 14.98331763 08
| Epoch (UTC): | 25 May 2026 08:27:50 |
| Eccentricity: | 0.0003154 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 131.2933° |
| argument of perigee: | 269.7394° |
| revolutions per day: | 14.98331763 |
| mean anomaly at epoch: | 90.3404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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