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 55410U 26145.57935723 +.00000000 +00000-0 +39919-4 0 00002
2 55410 69.9992 250.4194 0003459 269.0950 90.9813 14.98332487 07
| Epoch (UTC): | 25 May 2026 13:54:16 |
| Eccentricity: | 0.0003459 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.4194° |
| argument of perigee: | 269.0950° |
| revolutions per day: | 14.98332487 |
| mean anomaly at epoch: | 90.9813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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