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 55336U 26145.46158858 +.00000000 +00000-0 -86881-5 0 00005
2 55336 43.0029 215.1212 0001624 271.1677 88.8989 15.27581020 01
| Epoch (UTC): | 25 May 2026 11:04:41 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.1212° |
| argument of perigee: | 271.1677° |
| revolutions per day: | 15.27581020 |
| mean anomaly at epoch: | 88.8989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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